DocumentCode :
2985076
Title :
Terrain following/terrain avoidance path optimization using the method of steepest descent
Author :
Asseo, Sabi J.
Author_Institution :
Northrop Corp., Hawthorne, CA, USA
fYear :
1988
fDate :
23-27 May 1988
Firstpage :
1128
Abstract :
A path-optimization algorithm for terrain following/terrain avoidance and threat avoidance is presented. The algorithm uses the gradient method for generating the optimal ground track that minimizes a quadratic cost function of the aircraft´s altitude above sea level to maximize terrain masking while penalizing large deviations from a prescribed initial ground track. The vertical flight path for each ground track is obtained by using parabolic flight segments that satisfy vertical path constraints. Confining the optimization process to the horizontal plane improves the convergence properties of the algorithm, reduces the storage requirements, and allows the algorithm to be used on fine-grain terrain data. Simulation results are presented which validate the algorithm
Keywords :
aircraft; military computing; aircraft´s altitude; convergence properties; dynamic programming; fine-grain terrain data; gradient method; optimal ground track; optimization process; parabolic flight segments; path-optimization algorithm; quadratic cost function; simulation; steepest descent method; terrain avoidance; terrain following; terrain masking; vertical flight path; vertical path constraints; Acceleration; Aircraft; Constraint optimization; Convergence; Cost function; Dynamic programming; Gradient methods; Optimization methods; Sea surface; State-space methods;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Aerospace and Electronics Conference, 1988. NAECON 1988., Proceedings of the IEEE 1988 National
Conference_Location :
Dayton, OH
Type :
conf
DOI :
10.1109/NAECON.1988.195148
Filename :
195148
Link To Document :
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