A Computer Program for Aircraft Optimal Control Problems.
AIR FORCE ACADEMY COLO DEPT OF AERONAUTICS
Pagination or Media Count:
The report described uses a gradient technique having a rapid convergence rate to investigate problems of aircraft optimal control. The Fortran program for the Burroughs 6700 computer and sample output are included for a minimum time turn 3 dimensional for an aircraft with thrust vectoring capability. The operation of the program is explained and the program variables are identified. Author