ACMR/I System
International Telemetering Conference Proceedings / October 18-20, 1977 / Hyatt House Hotel, Los Angeles, California === The instrumentation system described provides real-time attitude and position data on 8 high-dynamic fighter aircraft and position data on 12 additional cooperative targets. Posit...
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International Foundation for Telemetering
1977
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ndltd-arizona.edu-oai-arizona.openrepository.com-10150-6097062016-05-20T03:01:35Z ACMR/I System Parker, J. Cubic Corp. International Telemetering Conference Proceedings / October 18-20, 1977 / Hyatt House Hotel, Los Angeles, California The instrumentation system described provides real-time attitude and position data on 8 high-dynamic fighter aircraft and position data on 12 additional cooperative targets. Position data is derived from multilateration range measurements using FM-CW phasecomparison techniques. Attitude and acceleration data is obtained from a strap-down inertial system initialized by the ranging system. Digital data is transmitted to and from the target by frequency shift keying of the ranging carrier. A multiprocessor ground computer using Kalman filter techniques provides a total state vector for each participant at a rate of 10 per second. The multiprocessor also provides real-time missile simulation for performance scoring. The Display and Debriefing Subsystem provides real-time computer-drawn pseudo three-dimensional display of the aircraft, total replay capability, and control of the entire system from the operator's console. 1977-10 text Proceedings 0884-5123 0074-9079 http://hdl.handle.net/10150/609706 http://arizona.openrepository.com/arizona/handle/10150/609706 International Telemetering Conference Proceedings en_US http://www.telemetry.org/ Copyright © International Foundation for Telemetering International Foundation for Telemetering |
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International Telemetering Conference Proceedings / October 18-20, 1977 / Hyatt House Hotel, Los Angeles, California === The instrumentation system described provides real-time attitude and position data on 8 high-dynamic fighter aircraft and position data on 12 additional cooperative targets. Position data is derived from multilateration range measurements using FM-CW phasecomparison techniques. Attitude and acceleration data is obtained from a strap-down inertial system initialized by the ranging system. Digital data is transmitted to and from the target by frequency shift keying of the ranging carrier. A multiprocessor ground computer using Kalman filter techniques provides a total state vector for each participant at a rate of 10 per second. The multiprocessor also provides real-time missile simulation for performance scoring. The Display and Debriefing Subsystem provides real-time computer-drawn pseudo three-dimensional display of the aircraft, total replay capability, and control of the entire system from the operator's console. |
author2 |
Cubic Corp. |
author_facet |
Cubic Corp. Parker, J. |
author |
Parker, J. |
spellingShingle |
Parker, J. ACMR/I System |
author_sort |
Parker, J. |
title |
ACMR/I System |
title_short |
ACMR/I System |
title_full |
ACMR/I System |
title_fullStr |
ACMR/I System |
title_full_unstemmed |
ACMR/I System |
title_sort |
acmr/i system |
publisher |
International Foundation for Telemetering |
publishDate |
1977 |
url |
http://hdl.handle.net/10150/609706 http://arizona.openrepository.com/arizona/handle/10150/609706 |
work_keys_str_mv |
AT parkerj acmrisystem |
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1718271948929105920 |