An Impact-Location Estimation Algorithm for Subsonic Uninhabited Aircraft

Bauer, Jeffrey E. and Teets, Edward (1997) An Impact-Location Estimation Algorithm for Subsonic Uninhabited Aircraft. Technical Report NASA/TM-97-206299, Research Engineering, NASA Dryden Flight Research Center.

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Abstract

An impact-location estimation algorithm is being used at the NASA Dryden Flight Research Center to support range safety for uninhabited aerial vehicle flight tests. The algorithm computes an impact location based on the descent rate, mass, and altitude of the vehicle and current wind information. The predicted impact location is continuously displayed on the range safety officer's moving map display so that the flightpath of the vehicle can be routed to avoid ground assets if the flight must be terminated. The algorithm easily adapts to different vehicle termination techniques and has been shown to be accurate to the extent required to support range safety for subsonic uninhabited aerial vehicles. This paper describes how the algorithm functions, how the algorithm is used at NASA Dryden, and how various termination techniques are handled by the algorithm. Other approaches to predicting the impact location and the reasons why they were not selected for real-time implementation are also discussed.

EPrint Type:	NASA Technical Memorandum
Keywords:	Flight termination, Flight testing, Impact prediction, Range safety, Uninhabited aircraft
Subjects:	Aircraft/Project: UAV (01 - 09) Aeronautics: (03) Air Transportation And Safety
ID Code:	162
Deposited On:	10 June 2004
Additional Information:	28 pages.