• 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