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Robust Missile Feedback Control Strategies

  • Published:2010-11 Issue:6 Volume:33 Page:1837-1846
  • ISSN:0731-5090
  • Container-title:Journal of Guidance, Control, and Dynamics
  • language:en
  • Short-container-title:Journal of Guidance, Control, and Dynamics

Author:

Trottemant E. J.1,Scherer C. W.2,Weiss M.3,Vermeulen A.4

Affiliation:

1. Delft University of Technology, 2628 CD Delft, The Netherlands

2. University of Stuttgart, 70569 Stuttgart, Germany

3. TNO Defence, Safety and Security, 2288 GJ Rijswijk, The Netherlands

4. Netherlands Defence Academy, 1781 AC Den Helder, The Netherlands

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

2. Optimality of robust disturbance-feedback strategies;International Journal of Robust and Nonlinear Control;2015-05-20

3. Robust Discrete-Time Proportional-Derivative Navigation Guidance;Journal of Guidance, Control, and Dynamics;2012-05
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