Title :
Developmental flight testing of a digital terrain system for the USAF F-16
Author :
Coleman, Capt Glenn ; Seelos, Michael ; McAllum, Capt Sean
Author_Institution :
U.S. Air Force Flight Test Center, Edwards AFB, CA, USA
Abstract :
The United States Air Force decided to integrate a Digital Terrain System into all F-16s to reduce the number of controlled flight into terrain mishaps. Through the use of a digital map of the Earth used in conjunction with the F-16´s own inertial navigation system and radar altimeter, the DTS provides the F-16 with an all-attitude, complete-envelope, ground and obstacle collision avoidance system with passive terrain following and bomb ranging capabilities. The F16 Combined Test Force at Edwards AFB, CA recently completed the second and final phase of the DTS development program. This flight test program spanned two years and flew over 150 test sorties. The system was shown to considerably reduce the pilot´s workload and increase situation awareness, especially at night, in low visibility conditions and low-level, high workload environments. In addition, it provided valuable ground and obstacle collision avoidance warnings that should decrease any further F-16 mishaps
Keywords :
aircraft control; aircraft displays; aircraft navigation; collision avoidance; head-up displays; inertial navigation; military aircraft; military avionics; COTS; HUD; USAF F-16; all-attitude; avionics; bomb ranging capability; complete-envelope; controlled flight into terrain mishaps; database terrain cueing; developmental flight testing; digital map; digital terrain system; ground collision avoidance system; inertial navigation system; obstacle collision avoidance system; passive terrain following; radar altimeter; situation awareness; Accidents; Aerospace electronics; Aerospace testing; Aircraft; Collision avoidance; Control systems; Costs; System testing; Visual databases; Weapons;
Conference_Titel :
Aerospace Conference, 1999. Proceedings. 1999 IEEE
Conference_Location :
Snowmass at Aspen, CO
Print_ISBN :
0-7803-5425-7
DOI :
10.1109/AERO.1999.789770