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Linear-quadratic guidance law for dual control of homing missiles

  • Published:1990-01 Issue:1 Volume:13 Page:137-144
  • ISSN:0731-5090
  • Container-title:Journal of Guidance, Control, and Dynamics
  • language:en
  • Short-container-title:Journal of Guidance, Control, and Dynamics

Author:

Hull D. G.1,Speyer J. L.1,Burris D. B.1

Affiliation:

1. University of Texas, at Austin, Austin, Texas

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering

Reference14 articles.

1. 2Larson, S. W. "Maximum Information Trajectory for an Air-to-Air Missile Intercept," M.S. Thesis,Univ. of Texas, Austin, TX, Dec. 1980.

2. Estimation enhancement by trajectory modulation for homing missiles

3. 4Tseng, C.Y. "A Study of Maximum Information Trajectories for Homing Missile Guidance," Ph.D. Dissertation,Univ. of Texas, Austin, TX, Dec. 1983.

4. Maximum-information guidance for homing missiles

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