DocumentCode :
2839105
Title :
Formation flight system design concept
Author :
Richardson, Cecil ; Schoultz, Michael
Author_Institution :
IBM, Owego, NY, USA
fYear :
1991
fDate :
14-17 Oct 1991
Firstpage :
18
Lastpage :
25
Abstract :
IBM recently completed a baseline design study for a formation flight system to be used for rendezvous, join-up, and formation flight of US Air Force helicopters and fixed-wing aircraft. The baseline system uses a Global Positioning System/inertial navigation system (GP/INS) relative navigation concept with backup data link range measurement as the basis of the precise position location for all aircraft both within the formation and among the separate formations. Part of the study included development of flight guidance algorithms for rendezvous of helicopters with tankers, joinup of individual aircraft into existing formations, and station-keeping within formation flight. The situational awareness display, guidance algorithms, and flight control cues have been demonstrated in a pilot-in-the-loop simulator and pilot comments have been favorable
Keywords :
aerospace computing; aircraft control; computerised navigation; Global Positioning System; IBM; US Air Force helicopters; backup data link range measurement; fixed-wing aircraft; flight guidance algorithms; flight joinup; flight rendezvous; formation flight system; guidance algorithms; inertial navigation system; pilot-in-the-loop simulator; relative navigation; situational awareness display; station-keeping; tankers; Aerospace control; Aerospace simulation; Aircraft navigation; Displays; Eyes; Global Positioning System; Helicopters; Military aircraft; Position measurement; Radar;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Digital Avionics Systems Conference, 1991. Proceedings., IEEE/AIAA 10th
Conference_Location :
Los Angeles, CA
Type :
conf
DOI :
10.1109/DASC.1991.177138
Filename :
177138
Link To Document :
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