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Optimum guidance with a single uncertain time lag

  • Published:1995-09 Issue:5 Volume:18 Page:981-988
  • ISSN:0731-5090
  • Container-title:Journal of Guidance, Control, and Dynamics
  • language:en
  • Short-container-title:Journal of Guidance, Control, and Dynamics

Author:

Yaesh I.1,Asher J. Z. Ben1

Affiliation:

1. TAAS Israel Industries, Ramat-Hasharon 77, Israel

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

Cited by 24 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Hit-to-kill accurate minimum time continuous second-order sliding mode guidance for worst-case target maneuvers;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2020-09-04

2. Practical generalized optimal guidance law with impact angle constraint;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2018-10-26

3. Synthesis of Robust Piecewise Affine Output-Feedback Strategies;Journal of Guidance, Control, and Dynamics;2016-07

4. Terminal guidance laws of missile based on ISMC and NDOB with impact angle constraint;Aerospace Science and Technology;2013-12

5. Shaping Guidance Law with Impact Angle Constraint for Alleviating Guidance Command at Terminal Phase;AIAA Guidance, Navigation, and Control (GNC) Conference;2013-08-15
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