Progress Update. RT Logic, Steve Williams. Operations Symposium & Exhibition 20 October, 2010

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Testing the Test Range without Flights Progress Update RT Logic, Steve Williams 48 th Annual Targets, UAVs and Range Operations Symposium & Exhibition 20 October, 2010 Colorado Springs, CO (719) 598-2801 Denver, CO (303) 703-3834 http://www.rtlogic.com

Whenever transmitters and receivers are in motion with respect to each other, RF link perturbations occur. Common Perturbations Signal Strength Delay Doppler shift Noise Interference Terrain Blockage Body shielding Weather Multipath Ducting Etc. Range TM Site Range TM Site 20 October, 2010 2

Signals TM1 and TM2 are transmitted from the same transmitter, so the data on each is the same, but the signals can look dramatically different from each other at receiving TM sites. TM1 Examples TM1 delay shorter than TM2 TM1 signal strength higher than TM2 TM1 affected by more Doppler shift than TM2 TM1 affected by different terrain than TM2 TM1 antenna angles different than for TM2 Etc. TM2 Range TM Site Range TM Site 20 October, 2010 3

A method for testing the Test Range without flights is to supply signals from a central fixed location to the TM sites that have these same signal characteristics. TM Data Source Test Controller, Time Sync TM1 Channel Channel Simulator Simulator TM2 Range TM Site Range TM Site 20 October, 2010 4

Examples TM1 delay shorter than TM2 TM1 signal strength higher than TM2 TM1 affected by more Doppler shift than TM2 TM1 affected by different terrain than TM2 TM1 antenna angles different than for TM2 Etc TM Data Source Test Controller, Time Sync TM1 Channel Channel Simulator Simulator TM2 Range TM Site Range TM Site 20 October, 2010 5

Signal Delay Variance Through Flight Gaps are terrain, link budget, and/or body shielding drop-outs Elapsed Mission Time (minutes : seconds) RF signals are received at each TM site at slightly different times due to the dynamic distance between the flight platform and the TM site location. 20 October, 2010 6

Attenuation (Loss) Variance Through Flight RF signals are received with differing i power levels at each TM site at due to the dynamic distance between the flight platform and the TM site location. Other dynamic attenuation factors include antenna patterns, body shielding, foliage, frequency selection, etc. Elapsed Mission Time (minutes : seconds) 20 October, 2010 7

Testing possibilities TM Site as a whole TM Site RF hardware elements TM Site signal processing hardware elements TM Site firmware, software, algorithms or processes Entire Test Range, including BSS, Range Control Center Displays and final data creation/processing Training possibilities TM Site Operators Range Operators Nominal conditions Worst-case conditions Up-front range capability proof to customer Range mission readiness proof to range personnel and customer 20 October, 2010 8

Theory is sound And, Channel Simulators do exist But usually used in the lab for testing flight/ground hardware, SW, FW, etc. Flight/Ground systems: Satellites, UAVs, Targets, Aircraft, Missiles, etc. 20 October, 2010 9

Channel Simulators haven t been used in this manner in the past. Will they be useful for Range Testing? With high power amplifiers and antennas With complex flight profiles and flight/ground antenna models Needed to find a Test Range and a flight capability that was interested in helping validate the concept. UTTR, Summer, 2009 Use of a Channel Simulator to pre-distort signals and transmit at RF to a TM site to validate received signal quality and Doppler, delay, loss and noise expectations. Pax River and Airtec, Sept 28-29, 2010 Expanded test of entire concept 20 October, 2010 10

Test Process utilized at Pax River 1. Perform Test Flight Transmitting simple, known, unclassified BER TM Close range and long range signal fading, BER High speed, close passes Doppler shift Various turn maneuvers body shielding Horizon terrain masking Record as-transmitted TM and TSPI on aircraft (truth data) Also captured at Pax TM sites Record TM & and signal characteristics at two TM sites St. Mary s Airport On Pax River 20 October, 2010 11

2. Process flight TSPI data to create Channel Simulator control model that mirrored the actual flight. Latitude, Longitude, Altitude, Yaw, Pitch and Roll Incorporate previously constructed Aircraft body model Aircraft antenna/transmitter model RF Model TM site antenna/receiver model 3. Use Channel Simulators to transmit to 2 TM sites. Input signal = BER TM pattern as recorded on aircraft during flight Use TSPI and RF model constructed in #2 above Record TM & signal characteristics at two TM sites 4. Compare TM & signal characteristics from actual flight (step #1) and the simulated (step #3) flight. 20 October, 2010 12

Airtec Beach A-100 King Air On board equipment rack GPS / IRIG Time BER / TM Data Generator S-Band Transmitter 20 October, 2010 13

Novatel ARDS Pod For acquiring recording and transmitting TSPI data 20 October, 2010 14

S-Band Antenna This was used for transmitting our test BER TM. A separate antenna was used for transmitting from the ARDS pod. 20 October, 2010 15

Antenna Body Shielding Mask Based on mounting location of antenna. Modeled d in AGI STK, which is used for Channel Simulator control. 20 October, 2010 16

Antenna Radiation Pattern Based on antenna characteristics. ti 20 October, 2010 17

Antenna Radiation Pattern and Body Shielding Mask Based on antenna characteristics ti and mounting location. 20 October, 2010 18

TM Sites This was the mobile site used at St. Mary s Airport Very similar system used at Pax River site. 20 October, 2010 19

TM Site locations for test flight 20 October, 2010 20

Test Flight, Pax River, 28 Sept, 2010 20 October, 2010 21

Flight Simulation, Pax River, 29 Sept, 2010 Primary Channel Simulation Equipment Telemetry Van Channel Simulators, Amplifiers and control elements. Two S-Band cone antennas pointed at 2 TM sites. 20 October, 2010 22

Very Preliminary Sample Data Altitude (meters) Scaled Relative Power (dbm) Without : -Antenna models -Body shielding -Antenna pointing error factoring -Time alignment -Etc Time (first ~15 minutes) 20 October, 2010 23

Near term next steps Continued data analysis Refine aircraft model, body masking and RF models Rerun test simulations in lab using collected TM data In-depth review of final results with Pax River Develop and implement recommendations Another test flight Retransmit to Pax TM sites Channel Simulator functionality modifications (e.g. multipath) Etc. 20 October, 2010 24

Summary Verification efforts continue, but Channel Simulators can be used to verify Test Range operation as a whole, or in part, and can be dual-purposed for Test Range operations training. Such testing/training is faster, more economical and more complete than testing/training with actual flights, since the limits of scenario development are virtually boundless. Acknowledgement RT Logic would like to express it s sincere gratitude to Mr. Bob Myers and his NAVAIR team at Pax River for their enthusiastic support and valued assistance in conducting these tests. For further information and/or a copy of the final report Steve Williams, RT Logic, 719-884-6269,. com Booth #315, NDIA Targets, UAVs and Range Operations Symposium. 20 October, 2010 25