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Telemetry Flight Data Recorders TSPI Measurement Flight Termination Power Systems Custom Products Avionics Solutions Product Catalog www.dynetics.com Dynetics Avionics Solutions 40 years of engineering excellence Save time and money while lowering risk with Dynetics avionics solutions. Founded in 1974 in Huntsville, Alabama, Dynetics has grown from a small, hometown company into a mid-tier provider of engineering, research, and development products and services to both government and private sector customers. Our 100% employee-owned company had sales of over $270 million and continues to expand an already broad range of solutions. Our mission is to deliver superior quality, hightechnology products and services ethically, responsively, and cost-effectively. As Dynetics continues to grow, both in size and capabilities, we will never grow beyond our commitment to our customers. This commitment is reflected by our vision to be the company of choice for customers who value high-technology products and services. y2 Dynetics offers a comprehensive suite of avionics solutions for the testing and evaluation of weapons systems. These highly configurable products are compact in size and cost-effective. Table of Contents ▪▪ Avionics Solutions Overview..................................................................4 Systems Modular Instrumentation System ▪▪ 2.75” Telemetry System...................................................................20 ▪▪ Telemetry System Highlights..................................................................6 ▪▪ Fuzewell Data Recorder..................................................................21 Building Block Modules ▪▪ FPS Flight Data Recorder................................................................22 ▪▪ Digital I/O PCM Encoder Module..........................................................7 ▪▪ 16-Channel Analog & Digital Input Module (3rd Gen.).................8 ▪▪ 12-Channel Universal Sensor Module.................................................9 ▪▪ High-Dynamic GPS Receiver Module............................................... 10 ▪▪ Miniature Inertial Measurement Unit (IMU)................................... 11 ▪▪ Power Converter Module...................................................................... 12 ▪▪ Analog Output Module.......................................................................... 13 ▪▪ Bidirectional Modem Interface Module........................................... 14 ▪▪ MIL-STD-1553 Bus Monitor................................................................... 15 ▪▪ Flight Termination Interface (FTI) Module...................................... 16 ▪▪ Flight Termination Receiver (FTR)...................................................... 17 ▪▪ Enhanced Flight Termination Receiver (EFTR)............................... 18 ▪▪ Single Fiber Transceiver......................................................................... 19 ▪▪ Flight Termination Products..........................................................23 ▪▪ TSPI Measurement Unit..................................................................24 ▪▪ MIS Flight Data Recorder................................................................25 ▪▪ Flight Video Recorder/Telemetry Module................................26 ▪▪ Flight Data Recorder........................................................................27 ▪▪ Integrated Telemetry System (5 Watts).....................................28 ▪▪ Ultra-Compact Telemetry (UCTM)...............................................29 ▪▪ Telemetry Instrumentation Portable Receiving Station (TIPRS)...................................................................................................30 ▪▪ Rotor Data Acquisition Systems (RDAS)....................................32 ▪▪ Isolated Power Controller Unit.....................................................33 ▪▪ OATIS.....................................................................................................34 ▪▪ Ground Station Support Services...............................................36 ▪▪ Flight Termination Receiver Test Set..........................................38 Configuration Tool ▪▪ Configure Your Own Instrumentation Systems.....................39 y3 Avionics Solutions The Modular Instrumentation System (MIS) is the core of Dynetics Avionics product line. The MIS provides custom capability with off the shelf products while providing a legacy of state of the art features and industry leading miniaturization. This catalog showcases the standard building block modules of the MIS product line as well as select examples of system level solutions. Configuration Tool The inside-back page offers a configuration tool to assist the user with configuring a system to support specific features and packaging options. Please feel free to contact Dynetics with any questions or specific configuration requests. High-Dynamic GPS Module Analog Input Module Basic & Enhanced Encoder Module Enhanced Inertial Measurement Unit (IMU) Module y4 Save time, money, and labor resources with the Dynetics MIS Dynetics MIS offers a comprehensive array of interchangeable and expandable modules that can be configured to meet customers’ unique requirements. Modules include: ▪▪ MIL-STD 1553 bus monitor ▪▪ Analog signal inputs ▪▪ Digital/discrete signal inputs ▪▪ Inertial measurements ▪▪ IRIG 106 custom encoding ▪▪ IRIG-B time code generator ▪▪ High-dynamic global positioning system (GPS) ▪▪ High-sensitivity GPS ▪▪ RF data transmission ▪▪ Onboard data storage ▪▪ Synchronous/asynchronous serial interface ▪▪ Time, space, and position information (TSPI) ▪▪ Secure communications ▪▪ Sensor Interface Flight proven in numerous missile environments, our comprehensive, compact design can often be installed without removing the warhead. Integration time is reduced with our system, making it more economical and cost-effective. The system delivers reliability and unique flexibility. Benefits: ▪▪ Many integration options ▪▪ Module interchangeability ▪▪ Ruggedized ▪▪ No mechanical moving parts ▪▪ Minimal wiring harnesses ▪▪ Custom solutions with commerical-off-the-shelf (COTS) components y5 www.dynetics.com Modular Instrumentation System (MIS) Telemetry System Highlights The MIS family provides a time, space, position information (TSPI)-capable telemetry unit or data recorder packaged in a ruggedized 2.5”-diameter housing capable of withstanding missile launches. The MIS telemetry system also includes power supply, signal conditioning, programmable encoder, transmitter, and dual-band conformal antenna. Modular design specifications (example configuration): ▪ Accepts additional MIS input modules Specifications ▪ Length: 14.1 cm (5.6 in) ▪ Diameter: 6.35 cm (2.5 in) Transmitter ▪ Weight: 610 g (1.36 lb) ▪ Other packaging and mounting options available Component Description Housing Precision-milled, specialized 2.5” x 5.5” canister missile firings and specially designed to house the MIS electronics Battery Rechargeable NiMH battery with nominal 1-hour operating life Transmitter 0.5-W to 5.0-W S-band, IRIG 106-compliant transmitter, tunable over the 2.2 to 2.95-GHz range Antenna Conformal wrap-around dual-band antenna for simultaneous telemetry and GPS operation Encoder module FPGA-based encoder with programmable frame structure, 6-pole premodulation filter, and 10-Mbit/sec output GPS module High-dynamic (50 g), C/A Code GPS with high update rates (15.625 Hz), 12-channel receiver, and L1 band operation IMU module MEMS-based miniaturized IMU with 3-axis variable range accelerometers, 3-axis rate sensors up to 1,200 deg/sec, 3-axis magnetometer, and temperature compensation Interface module High-density analog and sensor input modules available IMU module (optional) MEMS-based miniaturized IMU with 3-axis variable range accelerometers, 3-axis rate sensors up to 300 deg/sec, 3-axis magnetometer, and temperature compensation 1,200 deg/sec See page 39 for the Configuration Design Tool. ▪ ▪ ▪ ▪ Tunable 2250.5 to 2299.5 MHz Serial port programmable 500mW to 8W output Other options available Encoder ▪ User-programmable IRIG 106-compliant frame structure ▪ Bit rate 20 Mbps+ ▪ NRZL/RNRZL ▪ AES–128 Premodulation filter ▪ 6-pole Bessel Signal conditioning ▪ Analog • 16 differential inputs per module • Factory-adjustable gain • 5-pole Butterworth filtering ▪ Discrete • 8 TTL inputs • Logic-block processing ▪ Universal sensor ▪ 12 inputs per module ▪ GPS / IMU TSPI module • High-dynamic GPS • MEMS-based IMU Power source ▪ Rechargeable NiMH ▪ 55-minute operating time ▪ Other power options available 256.713.5060 • [email protected] • www.dynetics.com/products/instrumentation-and-telemetry y6 K140358_DS_telemetry sys 2014 Copyright. Dynetics, Inc. All Rights Reserved www.dynetics.com Modular Instrumentation System (MIS) Digital I/O PCM Encoder Module Specifications ▪ IRIG 106 Chapter 4 Compliant Frame Formats ▪ PCM Data Processing and Control ▪ Digital Programmable Premodulation Filter ▪ 25+ Mbps PCM Data Rate ▪ FPGA Based Processing ▪ Local Digital Temperature Sensor (1.5 deg C Accurate) ▪ GUI Programmable ▪ RS-232 Interfaces (2) ▪ RS-422/482 Interfaces (5) Highlights ▪ SDLC Interface Capable ▪ FPGA-based processing; easily configurable to provide custom telemetry solutions ▪ Up to 16 Discrete I/O Interfaces (Select Models) ▪ MIL-STD-1553 Data Bus Interface (Select Models) Temperature Sensor ▪ Many types of interfaces to meet a vast array of telemetry applications Flash Memory RAM MIS Module Interface User Programming GUI ▪ User-programmable through GUI RS-232 Interface Serial Interface Digitally Programmable Premodulation Filter FPGA PCM Processor SDLC RS-232 RS-422/485 16 Discrete I/O (Select Models) LVTTL/ RS-422/485 Output MIL-STD-1553 Interface (Select Models) PCM Output ▪ IRIG 106 compliant PCM frame structures ▪ Digitally programmable premodulation filter PCM Output ▪ Supports embedded synchronous/asynchronous serial streams ▪ Supports delayed data transmission ▪ Supports standard and custom band rates K140358 256.713.5060 • [email protected] • www.dynetics.com/products/instrumentation-and-telemetry 2016 Copyright. Dynetics, Inc. All Rights Reserved K140358_ Digital I/O PCM Encoder Module y7 www.dynetics.com Modular Instrumentation System (MIS) 16-Channel Analog & Digital Input Module (3rd Gen.) Specifications Programmable Analog Board A/D resolution ▪ 4 discrete inputs ▪ 8, 10, 12, 14, 16 bits ▪ Low noise levels ▪ >1 Mohm input impedance per channel Interface ▪ Compatible with MIS architecture ▪ -50 V to 50 V programmable discrete inputs with programmable hysteresis Physical dimensions ▪ Programmable (45-KHz maximum) fifth order switched capacitor filter ▪ Diameter: 2.375” min ▪ Programmable attenuation—capable of +/-50 V input in standard configuration (>50 V in special configurations) ▪ 16 differential or single-ended inputs ▪ Programmable differential signal offset (capable of moving differential signal DC component for higher resolution) Highlights ▪ Height: 1.248” min ▪ Weight: 120 g min Environmental ▪ Temperature sensor for temperature compensation Standard configuration capable of 250 KSPS ADC (up to and over 1 MSPS available through factory options; must bypass 45-kHz switched capacitor filter for higher frequency anti-aliasing). Microprocessor available for specific requirements or any additional processing. ▪ Programmable RC filter downstream of switched capacitor filter to block clock noise ▪ 1229 total components ▪ Programmable gain resistor on/off (value of gain resistor set at factory), providing the capability to add more resolution for small signals ▪ 18 PCB layers ▪ 4417 pins to 1111 pins/in2 ▪ 56 total feet of traces ▪ RS-422 TX and RX capability GUI programmable: All programmable parameters held in flash and programmable through encoder GUI interface (programs in 3 to 5 sec). Differential or single-ended analog output Programmable input attenuation (all pass included) >1 Mohm input impedance FPGA Programmable offset (negative, positive, or bi-polar signals) Programmable gain Fifth order switched capacitor filter ADC 256.713.5060 • [email protected] • www.dynetics.com/products/instrumentation-and-telemetry y8 K140358_Analog and Digital Input Module__16 Channel 2014 Copyright. Dynetics, Inc. All Rights Reserved www.dynetics.com Modular Instrumentation System (MIS) 12-Channel Universal Sensor Module Input configurable for common sensor types ▪ ▪ ▪ ▪ Analog measurements Thermocouples RTD Piezo-electric devices (Charge amplifier) ▪ IEP sensors (Constant current source) ▪ Bridge completion • Full / half / quarter • 3 to 4 wire Mix and match inputs at time of order Up to 16-bit resolution Sample rates to 1-M sample/sec 12 sensor channels ▪ Single ended or differential input ▪ 5 pole anti-alias filtering (1 to 45Khz) • Butterworth • Bessel • Elliptical ▪ ▪ ▪ ▪ Linearity better than 0.5% Programmable gain Programmable offset 10-mV to 50-V input range (range set at time of order) 5-V sensor excitation each channel Other excitation voltages available Highlights ▪ Custom firmware available ▪ Synchronous sampling ▪ RS422 interface (Rx/Tx) ▪ Effective Number of Bits (ENOB) tested >13 bits ▪ Standard configuration capable of 250 KSPS ADC (up to and over 1 MSPS available through factory options; must bypass 45kHz switched capacitor filter for higher frequency anti-aliasing) ▪ Microprocessor available for specific requirements or any additional processing GUI programmable: ▪ All programmable parameters held in flash and programmable through encoder GUI interface (programs in 3 to 5 sec) Part Number: # 10030319 256.713.5060 • [email protected] • www.dynetics.com/products/instrumentation-and-telemetry 2016 Copyright. Dynetics, Inc. All Rights Reserved K140358_DS_ultra compact telemetry y9 www.dynetics.com Modular Instrumentation System (MIS) High-Dynamic GPS Receiver Module This module provides the MIS with differential quality GPS capability at dynamic levels consistent with missiles and high-performance aircraft. When used as part of the Dynetics MIS TSPI system, sub-meter accuracy is achievable. Receiver RF front-end ▪ C/A L1 (1575.42 MHz) ▪ 12 parallel channels ▪ Gain: • 13.5 dB 1 stage Receiver type Low noise amplifier (LNA) RF reception sensitivity • 26 dB 2 stage ▪ -160 dBW ▪ Noise figure: 0.85 dB Signal acquisition Surface acoustic wave (SAW) filter ▪ 4 satellites: <3 sec ▪ All satellites in view (90%): <7 sec ▪ Absolute attenuation • L1 -40 MHz: 20 dB Time to first fix ▪ ▪ ▪ ▪ ▪ Hot: <1 sec Warm: <38 sec Cold: <45 sec Reacquisition: <0.5 sec Hybrid: <3 sec Maximum velocity ▪ >2000 m/sec (software limited) Maximum altitude ▪ 30,000 m (software limited) Highlights • L1 +40 MHz: 40 dB Interface ▪ Compatible with MIS architecture ▪ Compatible with data logger for logging application Physical ▪ Diameter: 2.375” min ▪ Height: 0.33” min ▪ Weight: 35 g min Maximum acceleration ▪ 25 g (navigation) ▪ 50 g (hybrid) Maximum jerk ▪ 500 g/sec for 100 msec (navigation) ▪ 500 g/sec for 100 msec (hybrid) Protocols ▪ RS-232 custom ▪ Navigation: PVTM, MACM ▪ Hybrid: 8003 RF Input LowPass Filter LNA SAW Filter Update rate ▪ 15.625 Hz (64 msec) Data redundancy ▪ Current and delayed GPS information ▪ Forward-error correction To MIS Bus FPGA GPS Receiver ▪ Onboard real-time GPS positioning ▪ Acquisition and tracking under very high accelerations with fast time to first fix ▪ High-accuracy differential positioning capable in realtime or for post-mission analysis ▪ Sends current GPS data, delayed GPS data, and forward-error correction This module can be used in navigation mode at up to 25-g acceleration. It can also be used as part of a hybrid GPS system when combined with the ground segment processor. In hybrid mode, code and carrier phase measurements are produced in the mobile receiver, with the navigation solution reconstructed in the ground segment. In this mode, the receiver can obtain fix in 1.5 sec (typical) and track at up to 50-g acceleration. 256.713.5060 • [email protected] • www.dynetics.com/products/instrumentation-and-telemetry y 10 K140358_High Dynamic GPS Receiver Module 2014 Copyright. Dynetics, Inc. All Rights Reserved www.dynetics.com Modular Instrumentation System (MIS) Miniature Inertial Measurement Unit (IMU) Triaxial low-noise accelerometers ▪ ▪ ▪ ▪ +/-35- or +/-50-g measurement ranges in lateral axes +/-35-, +/-50-, or +/-70-g measurement ranges in longitudinal axis 12-mg resolution in lateral axes; 16-mg resolution in longitudinal axis Internal self-test of MEMS sensors on power up 3-Axis Magnetometer Analog to Digital 3-Axis Accelerometer Analog to Digital Data Buffer To MIS Bus Triaxial rate gyros and triaxial magnetometer ▪ Up to 1200 deg/sec measurement range in yaw, pitch, and roll (other ranges available by request) ▪ 0.12 deg/sec resolution ▪ 0 to 40-Hz measurement bandwidth to 400-Hz measurement bandwith (variable) ▪ Internal self-test of MEMS gyro on power up ▪ +/- 6 gauss ▪ Integrated temperature sensor 3-Axis Magnetometer 3-Axis Gyro Analog to Digital Data Buffer To MIS Bus 3-Axis Accelerometer Interface ▪ 14 bits at > 50 kSPS (variable) ▪ Compatible with MIS architecture Physical dimensions Accelerometer specifications ▪ Diameter: 2.375” min ▪ Height: 0.316” min ▪ Weight: 120 g min ▪ +/-35- or +/-50-g measurement ranges in lateral axes ▪ +/-35, +/-50, or +/-70-g measurement ranges in longitudinal axis ▪ 14-bit resolution ▪ 2.5 mg/sqrt (Hz) ▪ RMS bias 10 mg ▪ Sensor misalignment 2° ▪ Scale factor error 0.1% ▪ Anti-alias filter cutoff 40 Hz to 400 Hz ▪ Configurable sample rate 1,000 Hz ▪ ▪ ▪ ▪ ▪ +/-1,200 deg/sec measurement range 14-bit resolution Sensor misalignment 2° Scale factor error 0.1% Anti-alias filter cutoff 40 Hz up to 400 Hz ▪ Configurable sample rate up to 50 kHz This module provides the MIS with inertial measurement capability for high-dynamic applications such as missiles or high-performance aircraft. Low-cost MEMS sensors are used to measure accelerations and rates around three orthogonal axes. A tri-axis magnetometer is also provided. Highlights include: Resolution Rate sensor specifications Highlights ▪ Simultaneous sampling of all channels ▪ Availability of custom dynamic ranges This module works in concert with the Dynetics MIS PCM encoder /data recorder and power supply modules to provide a complete data acquisition solution. 256.713.5060 • [email protected] • www.dynetics.com/products/instrumentation-and-telemetry 2014 Copyright. Dynetics, Inc. All Rights Reserved y 11 www.dynetics.com Modular Instrumentation System (MIS) Power Converter Module The power converter module provides power conditioning as necessary to meet MIL-STD 704A and MIL-STD-1275E power quality standards as well as EN55022, CISPR22, Class B EMI Compliant. This module contains an isolated DC-DC converter, two buck-boost regulators, a non-isolated DC-DC converter for MIS power, a LDO for low noise MIS power, EMI filters, inrush protection, reverse input protection, input diode isolation, short circuit protection, and power distribution that will convert the externally-supplied power to clean, filtered, regulated voltage levels necessary to power the entire MIS stack. It is also capable of supplying power to external devices such as transmitters, transponders, remote MIS stacks, etc. Specifications ▪ ▪ ▪ ▪ ▪ ▪ ▪ ▪ ▪ ▪ ▪ Provides clean, low-noise power for all MIS modules (up to 20W). High efficiency regulators (up to 98% efficiency). There is a total of 4 different diode ORed input powers, 2 battery and 2 external. All 4 inputs have reverse voltage protection, surge voltage protection, and soft starts. Only one of the external power inputs has spike protection. Can boost any of the 4 input voltages up to 40V with a maximum output of 10W from each buck-boost. There is a total of 9 different outputs. Each one is rated for at least 2A that can provide positive and/or negative voltages for MIS modules or external devices. One of the 9 power outputs can be controlled on or off at will by other modules in the MIS stack and can output any of the input/output voltages. The batteries can be turned on by applying voltage to a single pin. This feature can be configured to either be latched on by a momentary voltage or can be required to have a continuous voltage. The batteries can be turned on or off from other modules in the stack even when the batteries are isolated from MIS power. All power inputs can be isolated from the MIS module power and from each other or have various grounding schemes depending on their usage. A single discrete input that can be configured to accept an external input or that can be used to monitor battery voltage to provides status when the battery is on. Field Steady State Voltage Surge Voltage Spikes Non-operational Steady State Voltage Maximum Inrush Short Circuit Protection EMI Highlights ▪ Clean, low-noise power for all MIS modules (up to 20W). ▪ High efficiency regulators (up to 98% efficiency). ▪ Reverse voltage protection, surge voltage protection, and soft starts. ▪ Single discrete input Description 9.0 to 60.0 VDC (4.0 to 40.0 VDC with Buck-Boost) MIL-STD-704A, Figure 9, Limit 1& MIL-STD-1275E MIL-STD-704A, Figure 17 & MIL-STD-1275E 0 to 9.0 VDC (0 to 4.0 VDC with Buck-Boost) Limited with Soft Start Any Duration (200ms recovery time) EN55022, CISPRSS, Class B EMI Compliant 256.713.5060 • [email protected] • www.dynetics.com/products/instrumentation-and-telemetry y 12 K140358_ Power Converter Module 2016 Copyright. Dynetics, Inc. All Rights Reserved www.dynetics.com Modular Instrumentation System (MIS) Analog Output Module The MIS analog output module offers 16 outputs that can be factory configured to be single-ended or differential. Each channel is triggered or controlled individually to output set waveforms or receive waveforms remotely. The data is latched to each individual output synchronously for all 16 channels. The module is also designed to be able to either float the outputs when desired or to pullup each respective output to a known power rail. This feature allows the board to also be used in a digital / discrete output fashion. This capability also keeps the DAC outputs from having an unintended effect on external circuitry when not in use. The analog output module gives the MIS user the ability to output complex analog signals or to add an analog signal to an existing externally applied signal. This feature is useful for using the instrumentation system to augment flight testing or to aid in experiments. Specifications ▪ ▪ ▪ ▪ ▪ ▪ ▪ ▪ ▪ 16 output channels 16-bit resolution 1µs settling time 50 Mhz SPI communication to onboard DACs ±30 V to +60 V operation 10 mA/channel drive On/off function with pullup/down Less than 10 µV/°C temp drift -40 to +85°C operating Highlights ▪ Synchronous triggering available for all 16 channels ▪ Factory programmable waveforms • Polynomial • 18 kb block RAM per channel ▪ Internal/external clocking options available ▪ RS422 interface (Tx/Rx) ▪ Outputs on/off (floating, pullup, pulldown) ▪ Works with any MIS system 256.713.5060 • [email protected] • www.dynetics.com/products/instrumentation-and-telemetry 2015 Copyright. Dynetics, Inc. All Rights Reserved K140358_Enhanced Flight Termination Receiver y 13 www.dynetics.com Modular Instrumentation System (MIS) Bidirectional Modem Interface Module The bidirectional modem interface module allows the MIS system to transmit and receive data over commercial frequency bands. The MIS can be configured with controls that allow uplinked commands to be implemented. Specifications ▪ MIS-based encoder ▪ Control outputs • FET switches ▪ Frequency-hopping spread spectrum modem • 900 MHz • 2.4 GHz • 3.4 GHz ▪ AES 128 encryption ▪ 1 W power output (approx. 30-mile range) ▪ Up to 1.2 Mbps data rate Applications ▪ UAV ▪ Towed test vehicles ▪ Any application that requires lower data rates and non-irig frequency applications 256.713.5060 • [email protected] • www.dynetics.com/products/instrumentation-and-telemetry y 14 K140358_Bidirectional Modem Interface 2014 Copyright. Dynetics, Inc. All Rights Reserved www.dynetics.com Modular Instrumentation System (MIS) MIL-STD-1553 Bus Monitor The Dynetics MIL-STD-1553 MIS module allows insight into critical system operation during flight by monitoring and capturing 1553 bus message traffic. Specifications 1553 Interface ▪ 1553 A/B, STANAG 3838 ▪ Dual receivers for monitoring dual redundant links ▪ Integral isolation transformers ▪ Monitor terminal (MT) operation ▪ Double buffered data Monitoring Highlights ▪ Selective message monitoring / filtering based on message remote terminal (RT) address, transmit / receive, and subaddress Selectively filtered 1553 messages can be transmitted via a PCM telemetry stream or logged to nonvolatile memory as part of the Dynetics MIS small formfactor instrumentation system solution. ▪ User programmable CHANNEL A CH A COMMANDS RECEIVER A MESSAGE FILTERING CH A DATA (USER CHANNEL B PROGRAMMING) RECEIVER CH B TO MIS BUS COMMANDS B CH B DATA Physical dimensions ▪ Diameter: 2.375” min ▪ Height: 0.59” min ▪ Weight: 40 g min 256.713.5060 • [email protected] • www.dynetics.com/products/instrumentation-and-telemetry 2014 Copyright. Dynetics, Inc. All Rights Reserved K140358_Bus Monitor y 15 www.dynetics.com Modular Instrumentation System (MIS) Flight Termination Interface (FTI) Module Specifications ▪ MIS becomes infastructure of Flight Termination System (FTS) Power/ Control/Status Interface ▪ Implements one channel • Uses two modules for redundant system ▪ RCC-319 compliant ▪ FTS housekeeping ▪ MIS TM isolated interface—TM failure does not affect FTS ▪ Power management • Initiates thermal batteries—up to three—5 A, 36 V • Distributes power ▪ Isolated critical signal routing ▪ Internal or external Flight Termination Receiver (FTR) ▪ Integral controller ▪ Integral diagnostics/status serial output ▪ Pin compatible with commercial off-the-shelf (COTS) FTR and Flight Termination Safe and Arm (FTSA) designs FTR Interface FTSA Interface MIS Telemetry Interface Highlights The MIS FTI module allows for compact, reliable integration of flight termination components with the MIS telemetry system. When inserted into the MIS telemetry stack, the FTI provides power distribution, instrumentation and control, telemetry monitoring, health monitoring, and signal routing. ▪ Environmental ▪ Dependant on mounting ▪ Temperature: • -40 oC to +85 oC operating • -54 oC to +85 oC storage 256.713.5060 • [email protected] • www.dynetics.com/products/instrumentation-and-telemetry y 16 K140358_Flight Termination Interface Module 2014 Copyright. Dynetics, Inc. All Rights Reserved www.dynetics.com PRELIMINARY Modular Instrumentation System (MIS) Flight Termination Receiver (FTR) The Dynetics family of Flight Termination products leverages over 20 years of experience in missile and aircraft testing. The products are unique as they utilize the latest in electronics design and manufacturing technology to provide increased reliability, better performance, and features to aid the end user with integration. A standalone package compliant with the RCC-319 packaging requirements provide a drop-in replacement for legacy designs. A unique, compact integrated package is available for embedding the receiver within a Modular Instrumentation System (MIS) telemetry or recorder system. This configuration can be used with the MIS Flight Termination Interface (FTI) module that handles the interface, signal distribution, and instrumentation required for RCC-319 based Flight Termination Systems. The receivers also incorporate a unique serial status message that provides additional insight into the status and condition of the receiver system. Specifications ▪ ▪ ▪ ▪ ▪ ▪ ▪ ▪ ▪ ▪ ▪ ▪ MIS Form Factor Direct RF sampling (all-digital processing) Implements a single channel in a compact size RCC319 compliant Covers 405-450 MHz RF input with factory selectable 15 MHz band Dynamic Range: +13 dBm to less than -107 dBm All Digital FPGA-based Signal Processing, Downconversion, Filtering, Demodulation, Tone Detection, and Tone Decoding Comprehensive self-status and health monitoring Integral diagnostic serial port Pin compatible with commercial off-the-shelf (COTS) FTR designs Integrated serial interface to Dynetics FTI provides critical real-time FTR status and health information Factory Preprogrammed Center Frequency and Tone Frequencies Temperature: –40 oC to +85 oC operating; –54 oC to +100 oC storage BDES Key (EFTR) RF Input System Parameter Loading (EFTR) RF Front End (Amps, Filters, AGC) System Setup Parameters Diagnostic Data (RS-232) Analog-ToDigital Converter Digital Downconversion and Filtering Digital Demod System Status (RF Parameters, Voltage Readings, System Temperature, Measured Power, Etc.) FTR: Tone Detection EFTR: Decryption, Serialization Both: Command Decoding System Status and Health to FTI Dynetics provides the highest quality compact instrument and telemetry and is pleased to introduce the industry’s most flexible Flight Termination Receiver. Due to its alldigital nature, each FTR unit is can be factory upgraded to an Enhanced Flight Termination Receiver. Highlights The FTR features: ▪ Tone compatible ▪ MIL-STD-461 and RCC-319/RCC313 compliant Commands and System Outputs to FTI/FTSA ▪ Frequency range: 405 to 450 MHz ▪ Sensitivity: –115 dBm ▪ All digital, solid-state design ▪ COTS or custom/integrated packaging ▪ Factory programmable and reprogrammable K140358 256.713.5060 • [email protected] • www.dynetics.com/products/instrumentation-and-telemetry 2016 Copyright. Dynetics, Inc. All Rights Reserved K140358_Flight Termination Receiver y 17 www.dynetics.com Modular Instrumentation System (MIS) Enhanced Flight Termination Receiver (EFTR) The Dynetics family of Flight Termination products leverages over 20 years of experience in missile and aircraft testing. The products are unique as they utilize the latest in electronics design and manufacturing technology to provide increased reliability, better performance, and features to aid the end user with integration. The all-digital design can implement the latest Enhanced Flight Termination Receiver (EFTR) standard that incorporates an encrypted command link for mission security. A standalone package compliant with the RCC-319 packaging requirements is a drop-in replacement for legacy designs. An unique integrated package is available for embedding the receiver within a Modular Instrumentation System (MIS) telemetry or recorder system. Either configuration can be used with the MIS Flight Termination Interface (FTI) module that handles the interface, signal distribution, and instrumentation required for RCC-319 based Flight Termination Systems. The receivers also incorporate a unique proprietary serial status message that provides additional insight into the status and condition of the receiver system. Specifications ▪ ▪ ▪ ▪ ▪ ▪ ▪ ▪ ▪ ▪ ▪ ▪ All-digital Implements a single channel in a compact size RCC319 compliant Covers 405–450 MHz RF input with factory selectable 15 MHz band Dynamic range: +13 dBm to less than -107 dBm All -digital FPGA-based signal processing, demodulation, decoding, and command deciphering Comprehensive self-status and health monitoring Integral diagnostic serial port Pin compatible with commercial off-the-shelf (COTS) EFTR designs Externally programmable system parameters Integrated serial interface to Dynetics FTI provides critical real-time EFTR status and health information Temperature: –40 oC to +85 oC operating; –54 oC to +85 oC storage Highlights The EFTR features: ▪ EFTS (Enhanced Flight Termination System) ▪ Embedded Triple Data Encryption Standard (TDES) ▪ MIL-STD-461 and RCC-319/RCC313 compliant ▪ Frequency range: 420 to 450 MHz ▪ Sensitivity: –112 dBm ▪ Reed Solomon encoding ▪ All digital, solid-state design ▪ COTS or custom/integrated packaging 256.713.5060 • [email protected] • www.dynetics.com/products/instrumentation-and-telemetry y 18 K140358_Enhanced Flight Termination Receiver 2014 Copyright. Dynetics, Inc. All Rights Reserved www.dynetics.com Modular Instrumentation System (MIS) Single Fiber Transceiver The MIS Optical Transceiver provides a high-speed, full duplex data link over a single fiber. It’s designed to interface directly with an MIS Encoder Module, but may be used as a stand-alone data link. Multiple options are factory configurable including data rates, transmitter power output, receiver sensitivity, transceiver signal interface, operational wavelengths, and fiber connection types. Highlights Factory Configurable Data Rates: Fiber Configuration Options: ▪ Low speed (< 155 Mbps) ▪ Single mode (9/125 μm) or multimode (62.5/125μm) fiber ▪ 155 Mbps ▪ 622 Mbps ▪ 1.25 Gbps Receiver Configuration Options: ▪ AC or DC signal coupling ▪ Optical input sensitivity options based on factory-selected bit rate ▪ SC, FC, or ST fiber connector types available Bi-Directional Single Fiber Transceiver ▪ Single operational supply (+3.3V / +5V) ▪ Pigtail or receptacle ▪ Wide dynamic range receiver with AGC Physical dimensions ▪ Receiver signal detect functionality ▪ Diameter: 2.375” min ▪ Height: 0.60” min ▪ Weight: 30g min ▪ Wide operational temperature range (-40°C to +85°C) • -34 to -30 dBm typical for 155 Mbps ▪ PECL/LVPECL logic interface • -24 to -28 dBm typical for 622 Mbps ▪ 1310nm/1550nm or 1310nm/850nm operational wavelengths • -19 to -23 dBm typical for 1.25 Gbps Transmitter Configuration Options: ▪ AC or DC signal coupling ▪ Fabry-perot (FP) or distributed feedback (DFB) laser diode ▪ Multiple optical power outputs available • -15 to -8 dBm • -8 to -3 dBm • -3 to 0 dBm 256.713.5060 • [email protected] • www.dynetics.com/products/instrumentation-and-telemetry 2015 Copyright. Dynetics, Inc. All Rights Reserved K140358_Single Fiber Transceiver y 19 www.dynetics.com Modular Instrumentation System (MIS) 2.75” Telemetry System Self-contained warhead replacement telemetry system. Designed for use on the 2.75” size class of missiles and rockets such as Man Portable Air Defense Systems (MANPADS), Stinger, and Hydra 70. Provides telemetry of seeker data, inertial data, and position. Features ▪ Rechargeable battery ▪ High-dynamic GPS ▪ Programmable PCM encoder • L1-CA code ▪ Integral Antenna • 25 g navigation measurement • S-band telemetry • 50 g hybrid (raw) measurement • L1-GPS • 15.6 Hz raw data Highlights ▪ Internal/external power ▪ 16 V analog measurements ▪ Proven flight history on hundreds of missile test flights ▪ S-band transmitter • Programmable • Differential • 0.5 W to 1 W • 50 mV to 50 V • Programmable frequency ▪ Custom packaged to customer specification ▪ Flight motor initiation circuitry • 5-pole anti-alias ▪ Integrated design including: ▪ Custom packaging matched to customer ▪ 3-axis IMU • 3-axis accelerometer • Antenna • 3-axis rate sensor • Weight/CG • Batteries • 3-axis magnetometer • Mechanical packaging • Transmitter ▪ Run time up to 1 hour ▪ Compatible with all MIS modules ▪ Seeker/sensor integration available L1 Rechargeable Battery IMU GPS RS-422 Configuration 16 Analog Differential Analog Amp 4 Discrete 5-Pole Anti-Alias PCM Encoder S S-Band Transmitter K140358 256.713.5060 • [email protected] • www.dynetics.com/products/instrumentation-and-telemetry y 20 K140358_2.75” Telemetry System 2015 Copyright. Dynetics, Inc. All Rights Reserved www.dynetics.com Modular Instrumentation System (MIS) Fuzewell Data Recorder The Dynetics MIS-based fuzewell data recorder is a self-contained recorder system capable of simultaneously recording RS-232 serial data, MIL-STD-1553 bus traffic, and IRIG-106 PCM telemetry data. The unit features a rechargeable/replaceable battery pack, 16 GB of flash memory, USB 2.0 download capability, user-configurable PCM encoder, PCM output, premodulation filter, and IRIG time stamping. Designed for mechanical compatibility with several fuse packages, the recorder is intended to operate within a compliant fuzewell during captive carry conditions. Internally, the recorder has expansion slots and can be further customized at the factory for other applications by utilizing MIS input/output (I/O) modules. Configuration and control software allows system interface with a PC serial port for configuration and USB 2.0 for data retrieval and control. Fuzewell data recorder user panel interface The recorder is configured from existing MIS modules and specially packaged for a specific system application. The inboard end incorporates an integral battery pack, followed by a stack of MIS modules on circular circuit card assemblies. The outboard end incorporates an I/O interface panel including micro-D metal (MDM)style high density MIL-STD connectors, a radio frequency (RF) input for the GPS time synchronization, and a mini B USB port, in addition to three indicator lights. Highlights Specifications Component ▪ Self-contained data recorder Description ▪ Fits standard munitions fuzewell Size 7.48” length* x 2.88” diameter *Does not include connectors Weight 2.6 pounds Power Externally supplied MIL-STD-704E 28-V or internal rechargeable battery Battery 5-hour NiMH user replaceable Inputs MIL-STD-1553 PCM CLK/DATA RS-422 9600 Baud Serial ▪ 32-GB data storage Configuration Via user setup software GUI ▪ USB control and download Data download USB 2.0 ▪ Simultaneous recording of RS-232-serial data, PCM serial data, and MIL-STD1553 bus traffic ▪ Five-hour internal, rechargeable battery ▪ User configurable 256.713.5060 • [email protected] • www.dynetics.com/products/instrumentation-and-telemetry 2014 Copyright. Dynetics, Inc. All Rights Reserved K140358_DS_fuzewell data recd y 21 www.dynetics.com Modular Instrumentation System (MIS) GPS Flight Data Recorder The MIS family of products includes a data recorder module for non-telemetry applications. The MIS data recorder is the ideal solution for applications involving rugged environments and limited space for instrumentation. This product can be configured with any of the MIS modules (IMU, GPS, Analog, Sensor Acquisition, etc.) to form a complete instrumentation system. The data recorder module interfaces to the MIS bus and stores the collected data into nonvolatile memory. The stored data can be downloaded to a PC using a standard USB 2.0 interface Component Description Housing Precision-milled, specialized 2.5” by 5.5” canister capable of withstanding missile firings and specially designed to house the MIS electronics Battery Rechargeable NiMH battery with nominal 6-hour operating life Memory module 16-GB to 32-GB (expandable) memory Data download USB 2.0 (interface software provided) GPS module High-dynamic (50 g), C/A Code GPS with high update rates (15.625 Hz), 12-channel receiver, and L1 band operation IMU module (optional) MEMS-based miniaturized IMU with 3-axis variable range accelerometers, 3-axis rate sensors up to 300 deg/sec, 3-axis magnetometer, and temperature compensation 1,200 deg/sec Highlights ▪ Self-contained ▪ Interfaces to the full family of MIS instrumentation modules ▪ Compact ▪ Provides deep memory storage of data collections ▪ Simple USB interface for postmission data downloads ▪ Ideal for high-performance environments requiring high-speed instrumentation Specifications ▪ Drop-in self-contained GPS recorder • L1 C/A code receiver • Six-hour battery pack • Nine-hour flash memory • USB 2.0 download ▪ GPS only or GPS/IMU • Maximum velocity: 1900 m/sec (or > Mach 4)—software limited • Maximum acceleration: 25 g (standalone mode) and 50 g (hybrid mode) ▪ Differential reference groundstation (optional) • Maximum altitude: 30,000 m— software limited ▪ Post-processed data • Typical position real-time accuracy: <5 m (standalone mode) and <8 m (hybrid mode) • Submeter accuracy Reference Groundstation (optional) 256.713.5060 • [email protected] • www.dynetics.com/products/instrumentation-and-telemetry y 22 K140358_DS_gps flt data recd 2014 Copyright. Dynetics, Inc. All Rights Reserved www.dynetics.com PRELIMINARY Modular Instrumentation System (MIS) Flight Termination Products The Dynetics family of Flight Termination products leverages over 20 years of experience in missile and aircraft testing. The products are unique as they utilize the latest in electronics design and manufacturing technology to provide increased reliability, better performance, and features to aid the end user with integration. A standalone package compliant with the RCC-319 packaging requirements provide a drop-in replacement for legacy designs. A unique, compact integrated package is available for embedding the receiver within a Modular Instrumentation System (MIS) telemetry or recorder system. This configuration can be used with the MIS Flight Termination Interface (FTI) module that handles the interface, signal distribution, and instrumentation required for RCC-319 based Flight Termination Systems. The receivers also incorporate a unique serial status message that provides additional insight into the status and condition of the receiver system. Specifications ▪ ▪ ▪ ▪ ▪ ▪ ▪ ▪ ▪ ▪ ▪ ▪ Direct RF Sampling (All Digital Processing) Implements a single channel in a Compact size RCC319 compliant Covers 405-450 MHz RF Input with Factory Selectable 15 MHz Band Dynamic Range: +13 dBm to less than -107 dBm All Digital FPGA-Based Signal Processing, Downconversion, Filtering, Demodulation, Tone Detection, and Tone Decoding Comprehensive self-status and health monitoring Integral diagnostic serial port Pin compatible with commercial off-the-shelf (COTS) FTR designs Integrated serial interface to Dynetics FTI provides critical real-time FTR status and health information Factory Preprogrammed Center Frequency and Tone Frequencies Temperature: –40 oC to +85 oC operating; –54 oC to +100 oC storage BDES Key (EFTR) RF Input System Parameter Loading (EFTR) RF Front End (Amps, Filters, AGC) System Setup Parameters Analog-ToDigital Converter Digital Downconversion and Filtering Digital Demod System Status (RF Parameters, Voltage Readings, System Temperature, Measured Power, Etc.) FTR: Tone Detection EFTR: Decryption, Serialization Both: Command Decoding RCC-319 Compliant Package Dynetics provides the highest quality compact instrument and telemetry and is pleased to introduce the industry’s most flexible Flight Termination Receiver. Due to its alldigital nature, each FTR unit is can be factory upgraded to an Enhanced Flight Termination Receiver. Highlights The FTR features: ▪ Tone compatible ▪ MIL-STD-461 and RCC-319/RCC313 compliant ▪ Frequency range: 405 to 450 MHz ▪ Sensitivity: –115 dBm ▪ All digital, solid-state design ▪ COTS or custom/integrated packaging Commands and System Outputs to FTI/FTSA ▪ Factory programmable and reprogrammable System Status and Health to FTI Diagnostic Data (RS-232) K140358 256.713.5060 • [email protected] • www.dynetics.com/products/instrumentation-and-telemetry 2016 Copyright. Dynetics, Inc. All Rights Reserved y 23 K140358_Flight Termination Receiver www.dynetics.com TSPI Products Time Space Position Information (TSPI) Measurement Unit The MIS family of products includes an enhanced joint advance missile instrumentation (JAMI) TSPI unit. The TSPI measurement unit provides highly accurate position, velocity, and attitude information in high dynamic environments. The unit is fully compliant with existing JTU data formats and is fully interoperable with the existing JAMI real-time and post processing infrastructure. Building on flight proven MIS components, Dynetics offers a fully qualified TSPI measurement unit ready for fielding to meet your test & evaluation (T&E) requirements. Specifications ▪ Supports 28 VDC operation ▪ Fully compliant with JAMI infrastructure ▪ Fully compliant with the TSPI unit message structure (TUMS) ▪ Compact form factor ▪ Provides for external programmability ▪ Fully qualified off-the-shelf product, ready to be fielded Environmental Physical dimensions ▪ Shock: 4,750 g max ▪ Length: 4.58” ▪ Vibration: 5 g2/Hz max ▪ Width: 2.70” ▪ Operational temp.: -40 °C to 85 °C ▪ Height: 1.10” ▪ Storage temp.: -54 °C to 85 °C ▪ Weight: 1.1 lb ▪ EMI/EMC qualified Measurements ranges Highlights The TSPI measurement unit provides precise geo-location estimates through the use of both a GPS sensor unit and IMU. The TSPI measurementunit supports the serial data stream defined by the TSPI unit message structure (TUMS). The unit is externally programmable allowing for easy firmware modifications if and when changes are required. ▪ Rotational rate: ±500 deg/s, 0.05 deg/s/√Hz noise, 125-Hz output, 40-Hz bandwidth ▪ Linear acceleration: ±50 g, 2.5 mg/√Hz noise, 125-Hz output, 40-Hz bandwidth ▪ Velocity: 2000 m/sec max, 15.625-Hz output ▪ Position: 30,000 m altitude, 15.625-Hz output Accuracies ▪ 8-m RMS position accuracy (uncorrected)—20 cm (differential carrier phase) ▪ 1-m/sec RMS velocity accuracy (unblended) 256.713.5060 • [email protected] • www.dynetics.com/products/instrumentation-and-telemetry y 24 K140358_DS_TSPI measure unit 2014 Copyright. Dynetics, Inc. All Rights Reserved www.dynetics.com Modular Instrumentation System (MIS) MIS Flight Data Recorder A self-contained data recorder incorporating battery power, signal conditioning, control logic, sensor excitation and non-volatile data storage in a compact rugged canister. When powered on and activated the data is stored in flash memory that can be recovered post test via a USB 2.0 data port. Airborne Payload Interface/Controller ▪ 4.6Ahr Rechargeable NiMH battery (estimated runtime > 1 hour) ▪ Temperature monitor to prevent overcharging ▪ Power on/off via USB GUI or external momentary (1 sec min.) contact closure ▪ LED indicates “power on” ▪ Optional certification/testing to MILSTD-461F ▪ Controls power and recording ▪ Provides download interface ▪ Battery and memory status indicators Recorder/Memory ▪ 32 GB solid-state Flash ▪ USB 2.0 download (GUI download software included) ▪ Recorded file automatically saves if power removed (max. 60-sec data loss) ▪ Record initiated when power enabled ▪ LED and TTL indicator for “record” ▪ GPS time stamping on each measurement ▪ Accurate data begins recording within 1 sec of power on Inertial Measurement Unit (IMU) GPS Receiver ▪ C/A Code GPS receiver ▪ 15.6 Hz carrier phase, pseudorange, Doppler measurements ▪ 7 Hz Position, Velocity, Time Measurements (PVTMs) ▪ Velocity Limit > 1600 m/sec ▪ Altitude Limit > 30,000 ft ▪ Integral real-time clock ▪ LED and TTL indicator GPS lock status ▪ GPS signal locks within 10 sec of adequate signal Analog Sensor Module ▪ 24 inputs, 16-bit resolution (13 bit accuracy) ▪ +5-V excitation ▪ 4-wire bridge completion ▪ Sampling 2,000 to 20,000-Hz (factory configured) to customer specification ▪ Gains: 1, 2, 4, 5, 8, 10, 16 or 32 ▪ Specifications assume 350 Ω sensors Highlights ▪ Ruggedized self-contained data recorder ▪ 32 GB recording capacity ▪ Integrated MIS GPS, IMU, and analog sensor modules ▪ 24 external sensor inputs ▪ GPS time-stamping ▪ 4.6 Ahr rechargeable NiMH battery ▪ USB data download interface ▪ Acceleration: +/-50 G lateral axes, +/-70 G longitudinal axis ▪ Rate Sensors: +/-1,200 deg sec lateral and longitudinal axis ▪ 16 bit resolution, 13-bit accuracy ▪ 400 Hz per channel sampling/ 40 Hz anti-alias filtering 256.713.5060 • [email protected] • www.dynetics.com/products/instrumentation-and-telemetry 2016 Copyright. Dynetics, Inc. All Rights Reserved K140358_MIS Flight Data Recorder y 25 www.dynetics.com Modular Instrumentation System (MIS) Flight Video Recorder / Telemetry Module The flight video recorder / telemetry module is designed to support digital video. The encoder is factory configured to real-time parse the video data and extract a lower rate complete frame for telemetry while recording full data rate to the recoverable memory. The module has been used in the field to support a 640 x 480 camera and can simultaneously record 30 H of data and transmit 15 Mbps of telemetry. Applications ▪ Captive carry flight testing ▪ Laboratory testing ▪ Flight recovery testing Flight recorder electronics Highlights ▪ 150 Mbps recording capability ▪ Telemetry of selected video frames ▪ Real-time video viewer ▪ Integral 5 W transmitter (FM or SOQPSK) ▪ Integral battery ▪ USB download 256.713.5060 • [email protected] • www.dynetics.com/products/instrumentation-and-telemetry y 26 K140358_Flight Video Recorder Telemetry Module 2014 Copyright. Dynetics, Inc. All Rights Reserved www.dynetics.com Modular Instrumentation System (MIS) Flight Data Recorder The Dynetics MIS family of products includes a data recorder module for nontelemetry applications. The MIS data recorder is the ideal solution for applications involving rugged environments and limited space for instrumentation. This product can be configured with any of the MIS modules (e.g., IMU, GPS, analog, etc.) to form a complete instrumentation system. As the figure below shows, the data recorder module interfaces to the MIS bus and stores the collected data into nonvolatile memory. The stored data can be downloaded to a PC using a standard USB 2.0 interface. Specifications Data recorder module Memory characteristics ▪ USB 2.0 compliant with HID and bulk transfer support ▪ Up to 32 GB storage on each memory module ▪ External or USB trigger to toggle recording state ▪ Memory modules expansion allows up to 7 modules to be supported resulting in 56 GB storage Host HMI ▪ Recording speed at 147 Mbps ▪ USB communication performs memory management functions ▪ 10-year data retention ▪ Converts and parses data into customer-desired file format Data input ▪ 100,000 program/erase cycles ▪ Supports 8- or 16-bit input bus ▪ 3.3 V and 5 V compatible This configuration utilizes the Dynetics MIS as a data recorder. The system can be configured in any MIS package style and can utilize any of the modules of the Dynetics MIS system. The recorder configuration is self-contained and provides a cost-effective solution for non-destructive test applications. Highlights ▪ Provides simple USB interface for post-mission data downloads ▪ Interfaces to the full family of MIS modules ▪ 100-MHz data input clock ▪ Provides deep memory storage of data collections USB 2.0 MIS Bus FIFO ▪ Is ideal for rugged environments requiring highspeed instrumentation Data DataRecorder Logger Controller Controller ▪ Supports higher data rates than conventional telemetry Memory Bus DataRecorder Logger Module Data Module Memory Module Memory Module MIS data recorder successfully used in rocketball testing, where high-speed video was captured while the rocket was fi red down a steel cable. Nonvolatile Memory 1 Decoder Nonvolatile Memory 2 The MIS data recorder provides a complete MIS. 256.713.5060 • [email protected] • www.dynetics.com/products/instrumentation-and-telemetry 2014 Copyright. Dynetics, Inc. All Rights Reserved K140358_Data Recorder y 27 www.dynetics.com Modular Instrumentation System (MIS) Integrated Telemetry System (5 Watts) Overall Assembly Dynetics Part Number: 10029505 TM Module assembly Dynetics part number: 10029770 Weight 1.30 lbs (approximate) Battery Module assembly Dynetics part number: 10029771 Weight 1.41 lbs (approximate) Transmitter Module assembly Dynetics part number: 10029772 Weight 0.79 lbs (approximate) Specifications TM Module: Battery Module: ▪ Transmitter Module: ▪ 16 programmable channels o ¼ bridge 350 ohm Strain Gauges ▪ Nimh 1000 mAhr, 28.8-Vdc nominal ▪ 5 W (must heat sink) ▪ Minimum 50 minute runtime while transmitting at 5 W ▪ Selectable SOQPSK or PCMFM ▪ MMCX connection ▪ Derating and Discharge Curves: ▪ 600 mA at 28 Vdc ▪ GUI Configurable Encoder Frame Definition ▪ 130 mA @28 V ▪ Four internal expansion slots ▪ Highly tunable (output power, modulation, frequency, etc.) ▪ 2200.5 to 2394.5 MHz 256.713.5060 • [email protected] • www.dynetics.com/products/instrumentation-and-telemetry y 28 K140358_Demo TM Kit 2015 Copyright. Dynetics, Inc. All Rights Reserved www.dynetics.com Custom Telemetry Products Ultra-Compact Telemetry (UCTM) Building on Dynetics’ history of performance with small, compact telemetry (TM), our engineers have developed an ultra-compact TM (UCTM) solution to support very small missiles, munitions, or mortars. The UCTM utilizes existing technology proven through many years of flight testing. The UCTM offers the optimal solution for very tight form factor requirements. Specifications Highlights Features Environmental ▪ Compact form factor ▪ Operational temp.: -20 °C to 85 °C ▪ RS422 data input ▪ Storage temp.: -40 °C to 85 °C ▪ FPGA-based IRIG 106-compliant encoding ▪ Forward error correction Physical dimensions ▪ Low-power design ▪ Length: 1.0” • 0.25 W in standby mode • 2.5 W with transmitter • 3.3-VDC input The UCTM provides PCM encoding capability and forward error correction. The device includes an integrated lowprofile antenna. The transmitter frequency is user programmable and the UCTM supports high shock and acceleration environments. ▪ Width: 1.1” ▪ Height: 0.164” ▪ 1-Mbps output data rate ▪ Onboard transmitter • 250-mW power output • User programmable frequency from 2200.5 to 2290.5 MHz tunable in 1-MHz steps • Integrated low-profile chip antenna • FM modulation ▪ Built-in test provides transmitter status and output power estimate Part Number: 10011986 256.713.5060 • [email protected] • www.dynetics.com/products/instrumentation-and-telemetry 2014 Copyright. Dynetics, Inc. All Rights Reserved K140358_DS_ultra compact telemetry y 29 www.dynetics.com Ground Support Test Equipment Telemetry Instrumentation Portable Receiving Station (TIPRS) Highlights Fully integrated RF receiver, bit synchronizer, and decommutator ▪ S-band with 200 MHz tuning range ▪ Nominal – 70 dBm sensitivity ▪ 10 K – 10 Mbps data rate ▪ NRZ-L/M/S, RNRZ-L, bi-phase L/M/S Applications ▪ IRIG 106-compatible frame formats ▪ Laboratory testing ▪ IRIG B time code input ▪ Flightline checkout ▪ RS-422 clock and data outputs ▪ Covert data collection ▪ RS-422 clock and data inputs (optional) ▪ Quick response field test Ruggedized, self-contained system ▪ Remote site test ▪ Optional MIL-STD-461F compliant ▪ Shipborne testing ▪ Full magnesium alloy case ▪ Shock-protected removable HDD; vibration and drop resistant ▪ Battery or AC power operation with battery backup ▪ In-flight data collection ▪ System integration test ▪ Easy-to-carry and set up; ideal for flightline checkout or systems integration tests Optional data processor module Optional data processor module, port and size comparison 256.713.5060 • [email protected] • www.dynetics.com/products/instrumentation-and-telemetry y 30 K140358_TIPRS 2014 Copyright. Dynetics, Inc. All Rights Reserved. www.dynetics.com Ground Support Test Equipment TIPRS (Cont.) Specifications Operation ▪ Sunlight readable 14.1" screen ▪ Operating temp.: 32 °F to 140 °F / 0 °C to 60 °C (optional low temp.: -4 °F / -20 °C) ▪ Intel core duo 1.66 GHz processor, 4 GB DDR-II RAM ▪ Fanless IP54 sealed magnesium alloy die-cast chassis ▪ Storage temp.: -40 °F to 158° F / -40 °C to 70 °C ▪ Individually sealed ports ▪ Humidity: 5% to 95% RH, non-condensing ▪ Waterproof rubber keyboard, touch-sensitive control pad Physical dimensions ▪ XGA color TFT LCD 1024x768 resolution display, 64 MB shared VRAM ▪ Dimensions: 13.1” x 11.0” x 5.25” ▪ Removable 120 GB SATA HDD and DVD-RW combo drive module ▪ Weight: 17.0 lb ▪ Internal swappable rechargeable 9600 MaH Li-Ion battery pack ▪ Integrated 32-bit 3D/2D GFX-core with dynamic video memory technology BNC Antenna Not Supplied SMA IRIG B Input S-Band Receiver Bit Sync Sun Light Readable Display Optional Data Processor Decom IRIG B PC Interface Removable Battery Removable Hard Drive Rear Panel RS-422 Clock and Data TIPRS Block Diagram 256.713.5060 • [email protected] • www.dynetics.com/products/instrumentation-and-telemetry y 31 2014 Copyright. Dynetics, Inc. All Rights Reserved. www.dynetics.com Modular Instrumentation System (MIS) Rotor Data Acquisition Systems (RDAS) For over 20 years, Dynetics has been involved in the design, fabrication, and support of custom telemetry instrumentation systems. These systems have operated under harsh conditions varying from high frequency vibration to exposure to explosive atmosphere, rapid altitude changes, pressure changes, high spin rates, and low and high temperatures. Leveraging Dynetics’ proven MIS hardware, Dynetics has developed a rotor data acquisition system (RDAS). The RDAS provides an instrumentation unit to collect data and telemeter that data to a nearby fuselage receiver, avoiding costly onboard slip rings. The compact design of the system often allows for integration within the spinner or between rotor blades for rotor applications. An optional Dynetics-provided receiver and bit synchronizer in the fuselage can provide clock and data inputs for use by the decom and data recorders. Multiple antenna configuration options are available. The RDAS architecture is designed to be configurable to meet different data collection requirements and minimize non-recurring engineering (NRE) costs. Specifications ▪ Flexible communication link to fuselage (IRIG 106 S-band, with support for serial at 900 MHz spread spectrum or Ethernet) ▪ Configurable transmitter with low power consumption (typically S-band) On-axis rotating data acquisition provides scalable instrumentation. Typical Environments ▪ Operating temperature -20°C to 60°C ▪ Storage temperature -20°C to 50°C ▪ Humidity up to 100% ▪ Variable transmitter power (100 mW to 1W) ▪ Rotorcraft main and tail vibration ▪ User-programmable, IRIG 106-compliant encoder ▪ Altitude up to 25,000 feet ▪ Immersion up to 1 meter ▪ External or internal bridge completion (support for 1/4, 1/2, and full bridge) ▪ Internal 1/rev and Azimuth module ▪ Capable of supporting multiple bridge completion, analog/discrete inputs, and GPS ▪ Integrated power options for +28 V operation, battery operation, and onboard battery charging ▪ Weight varies with battery and data collection options (1 lb to 5 lb) ▪ Scalable size support data collection options • Diameter: 3” • Length: 5” to 9” Distributed data acquisition supports main and tail rotor environments. Support for MIS modules ▪ Sensor module ▪ Encoder module ▪ GPS and time module ▪ Battery charger ▪ Battery monitor ▪ Analog input module 256.713.5060 • [email protected] • www.dynetics.com/products/instrumentation-and-telemetry y 32 K140358_Rotor DARS 2015 Copyright. Dynetics, Inc. All Rights Reserved www.dynetics.com Power Conditioning Isolated Power Controller Unit Input Power: ▪ ▪ ▪ ▪ Three ideal diode OR’ed 28VDC inputs One input protected to MIL-STD-1760 Operation for all three inputs from 16 to 35 VDC Continuous input current capacity of > 4.25A. Output Power: ▪ Four controllable power 28VDC outputs ▪ 3 outputs that dispense the greater of the three 28VDC inputs capable of > 2.7A each ▪ 1 Isolated 28VDC DC/DC output capable of > 1A ▪ Triggered from programmable discrete inputs ▪ Discrete Outputs ▪ Two 28VDC outputs intended for status ▪ Low current outputs ▪ Triggered from programmable discrete inputs Power Control: ▪ Seven discrete inputs with programmable transition thresholds ▪ Programmed to control power and discrete outputs LVDS: ▪ Isolated two channel LVDS repeater ▪ Input isolated ▪ Output referenced to 28VDC input gnd Monitors: ▪ ▪ ▪ ▪ ▪ ▪ ▪ ▪ ▪ Highlights ▪ Power regulation, switching, monitoring, and isolation ▪ Compact, rugged, flightproven design ▪ Aids integration of instrumentation systems ▪ Programmable ▪ 7 Amp capacity ▪ Isolation < 2uA with ±40VDC applied across isolation barrier Current and Voltage monitors Total input current monitor (0-5V corresponds to 0-7A) 28VDC input voltage monitors for all three inputs Unit Temperature (0 to 5V corresponds to -40 to 100 deg C Programmable Features: Input to outputs debouncing and delays Input to Output triggering Discrete Input thresholds External interface allows programmability after build Environment: ▪ ▪ ▪ ▪ -40 to 85 deg C operating temperature EMI (CE102, CS101, CS114, CS115, CS116, RE102, RE103) Isolation < 2 uA with ±40VDC applied MIL-STD-810 256.713.5060 • [email protected] • www.dynetics.com/products/instrumentation-and-telemetry 2016 Copyright. Dynetics, Inc. All Rights Reserved y 33 K140358_Isolated Power Control Unit www.dynetics.com Open Architecture for Telemetry and Instrumentation Systems (OATIS) Specifications The open architecture for telemetry and instrumentation systems (OATIS) was developed by Dynetics for the System Simulation and Development Directorate (SSDD). OATIS is modular and designed to make, log, and transmit inertial and various other measurement to a ground station. It includes two subsystems: Airborne payload Ground station ▪ Airborne control unit (ACU) ▪ Ground station server ▪ RF modem and blade antenna C-MIGITS III GPS/INS and antenna (optional) ▪ Control panel ▪ Smart sensor nodes (SSNs) ▪ Moving map display ▪ Real-time strip-charts ▪ Configuration editor OATIS has been installed in the following unmanned aircraft systems (UAS): ▪ Hunter: precision engagement collaboration process (PECP) completed for integration on Hunter. Flown on Hunter during flight test demonstrations in January 2005. ▪ Shadow: initial integration and partial mission capable (PMC) flights performed December 2006 at Redstone Arsenal (RSA). Range check flights (100 km) performed at RSA in January 2007. ▪ Other: installed on a total of five vendor prototypes to collect independent measurements for aerial vehicle (AV) performance analysis. Data acquisition The SSNs are a family of distributed data acquisition products responsible for signal measurement. These devices consist of modular components for signal conditioning, measurement, and communication. A network of SSNs is connected to the ACU via a network cable in a daisy chain topology. The nodes are placed in the UAS in close proximity to the signals to be measured. The distributed data acquisition architecture of OATIS simplifies installation and maintenance of test equipment by significantly reducing the amount of cable that must be routed through the airframe. y 34 OATIS provides the following benefits to the UAS flight test environment: ▪ An independent measurement system to assist in evaluating aircraft performance and system functionality ▪ A flexible data acquisition subsystem (DAS) that allows efficient integration of new sensors as new test measurement requirements are identified ▪ Situational awareness for the test conductor ▪ Real-time visualization of measurement data during flight www.dynetics.com OATIS System Overview Hardware system Software system Airborne control unit (ACU) Ground station server ▪ ▪ ▪ ▪ ▪ ▪ ▪ Data link control ▪ Telemetry distribution via TCP/IP ▪ Telemetry logging PC-104 stack Onboard logging: 16+ hrs Post-flight download via USB Backup battery (optional) Ethernet port 5.1 lb (7.2 lb w/ battery) Inertial navigation system (INS) ▪ ▪ ▪ ▪ C-MIGITS III from Systron Donner MEMS-based IMU 12-channel Jupiter GPS 1.7 lb Smart sensor node (SSN) ▪ 7 analog voltage channels ▪ Sample rate: 1 to 4 kHz ▪ CAN bus output and control 0.4 lb RF modem ▪ ▪ ▪ ▪ ▪ COTS Microhard MHX-920 900 MHz frequency hopping ~60-mile range with omni antennas 1 W output 0.8 lb Ground station ▪ ▪ ▪ ▪ COTS laptop (Windows XP) RF modem Omni antenna OATIS control panel software Control panel ▪ ▪ ▪ ▪ Pre-flight initialization of INS Data link status and control GPS time display Log time remaining display Moving map display ▪ ▪ ▪ ▪ FalconView based Real-time situational awareness Flight test planning Flight path verification Real-time strip-charts ▪ Real-time graphical display ▪ INS and analog data ▪ Calculated values (e.g., density altitude) In-flight monitoring ▪ ▪ ▪ ▪ Configuration Editor Configuration of SSNs In-flight adjustment of logging rates User labels for measurement channels Real-time telemetry client library ▪ Common client library for telemetry ▪ Rapid development of new clients ▪ Clients can be located anywhere on a TCP/IP network 256.713.5060 • [email protected] • www.dynetics.com/products/instrumentation-and-telemetry 2014 Copyright. Dynetics, Inc. All Rights Reserved K140358_OATIS y 35 www.dynetics.com Telemetry and Instrumentation Ground Station Support and Services Dynetics provides end-to-end telemetry solutions for our customers. This includes design and fabrication of custom telemetry instrumentation; installation of instrumentation in a variety of high-performance missiles, aircraft, and other systems; field test support and data collection; and post-test data analysis. In 2007, Dynetics developed the telemetry and instrumentation ground receiver station (TIGRS) van to provide total system support at any test range. The TIGRS van includes state-of-the-art telemetry receivers, test equipment, and real-time analysis tools. TIGRS includes a customer viewing area that allows our customers to view live tests and test results. Dynetics has more than 15 years of experience in the design, fabrication, and support of telemetry systems. Over the years, Dynetics has acquired extensive expertise and state-of-the-art capabilities for telemetry data collection and test-range ground support. Specifications Mobile dual-axis tracking antenna TSPI ground segment ▪ ▪ ▪ ▪ ▪ ▪ Survey-grade GPS reference receiver ▪ Joint advanced missile instrumentation (JAMI) ground segments ▪ Processor provides a differentially corrected post-processing solution ▪ On-site TSPI processing Two independent tracking systems Frequency: 1425 to 2400 MHz Aperture diameter: 4 ft Gain: 25 dB Polarization: simultaneous LHCP and RHCP ▪ Antenna feed: conical scan ▪ Pedestal slew rate: 30 deg/sec ▪ Pedestal acceleration: 60 deg/sec/sec Multiple receivers ▪ ▪ ▪ ▪ IRIG-B generator Multiple day / night cameras Frequency: 2200 to 2400 MHz Noise figure: <8 dB IF bandwidth: selectable Demodulation format: PCM/FM and SOQPSK ▪ Data rates: up to 20 Mbps High-speed digital satellite link Decom ▪ Video recording capabilities with IRIG-B timing overlay ▪ Customer viewing area ▪ Highly mobile and self-contained ▪ Independent power generation capability ▪ Simultaneous recording of multiple telemetered units ▪ Data rates: up to 20 Mbps ▪ Bit encoding: NRZ-L/M/S and biphaseL/M/S ▪ Network: ethernet TCP/IP ▪ Data storage capacity: 80 GB ▪ IRIG-B time-sync accuracy: +/-1 msec ▪ ENA gateway compatible y 36 ▪ Provides Internet and VOIP telephone service to remote locations Other features Highlights ▪ Experienced team ▪ Broad expertise in missile and unmanned systems testing ▪ Expertise in coordinating with multiple test ranges ▪ Extensive pre-mission and post-mission analysis ▪ Real-time results and quicklook analysis tools ▪ Redundant data collection to minimize data-collection failures ▪ Leading-edge GPS technology ▪ Test enabling network architecture (TENA) capability ▪ Custom data reduction ▪ Video capture of mission events www.dynetics.com Ground Station Support and Services (Continued) 256.713.5060 • [email protected] • www.dynetics.com/products/instrumentation-and-telemetry 2014 Copyright. Dynetics, Inc. All Rights Reserved K140358_Ground Station Support y 37 www.dynetics.com Ground Support Test Equipment PRELIMINARY Flight Termination Receiver Test Set Dynetics’ Flight Termination Receiver Test Set provides customers a sleek, convenient, and integrated test kit for Tone-Based FTR units by implementing the 313-01 ATP and recertification procedure. Additionally, it provides complex encoded and encrypted EFTR waveforms to aid in preliminary testing of EFTR units. The test unit is ideal for customers desiring to reduce the man hours required to recertify FTR units or for customers who desire a flexible and powerful waveform and tone generator for FTR and EFTR RF inputs. The DDS and FPGA based test unit allows for remote reprogramming and feature upgrades. A polished and user-friendly GUI provides the customer with ample controls and real-time status feedback data. The user is able to put the unit in both a manual control mode and an automated test mode, facilitating a variety of testing requirements. The Test Set unit is fully integrated, comprised of power supplies, digital circuitry, and RF circuitry. A standard 110V 60 Hz AC power input pulls less than 3 amps max. Highlights ▪ Portable integrated test kit All front panel connectors are industry standard, including an SMA cable for RF, a 25-pin Micro D for FTR/EFTR interface, a six-pin audio connector for keyload, and a durable power switch with LED for status power indication. ▪ Complex encoded and encrypted EFTR waveforms Features ▪ User-friendly GUI with realtime feedback data • Portable Integrated FTR Testing capability • Supports 405-450 MHz Band ▪ Remote programming and feature upgrades ▪ Reduces man-hours for recertification of FTR units • Output RF Power Level -120 dBm to + 13 dBm • SMA RF Output • User-friendly control and status GUI • Provides an automated 313-01 ATP and Cert/Recert capability for Tone-Based and FTR units • Capable of generating complex EFTR stimulus waveforms • Encryption keyload for EFTR TDES • Standard 25-pin Micro-D connector interface to FTR/EFTR unit 256.713.5060 • [email protected] • www.dynetics.com/products/instrumentation-and-telemetry y 38 K140358_Flight Termination Receiver Test Set 2016 Copyright. Dynetics, Inc. All Rights Reserved Configure Your Own Instrumentation System Flight Termination Interface 16-Channel Analog Signal Conditioner 16-Channel Analog Output PCM Encoder RS-422 I/O 2.375” Digital Data Bus Interface IRIG Time Generator Flight Termination Data Recorder 12-Channel Universal Sensor Multi-Mode Fiberoptic Interface 28V Power Conditioner 1553 Encoder Interface High Dynamic GPS Rechargeable Battery Pack 6DOF IMU Battery Power Conditioner Bidirectional Modem Connectors shown for size reference K140358 37 PIN NANO 37 PIN MDM www.dynetics.com/products/instrumentation-and-telemetry [email protected] 256.713.5060 www.dynetics.com K140358_Product Catalog Copyright 2015 Dynetics, Inc., all rights reserved