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Analytical solution of field-of-view limited guidance with constrained impact and capturability analysis

  • Published:2020-02 Issue: Volume:97 Page:105586
  • ISSN:1270-9638
  • Container-title:Aerospace Science and Technology
  • language:en
  • Short-container-title:Aerospace Science and Technology

Author:

Han Tuo,Hu Qinglei,Xin Ming

Funder

Major Project of Science and Technology Innovation 2030

Project of Science and Technology on Space Intelligent Control Laboratory

National Defense Basic Scientific Research Program of China

Academic Excellence Foundation of BUAA for PhD Students

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference34 articles.

1. Analytic solutions of generalized impact-angle-control guidance law for first-order lag system;Lee;J. Guid. Control Dyn.,2013

2. Terminal impact angle constraint guidance with dual sliding surfaces and model-free target acceleration estimator;Hou;IEEE Trans. Control Syst. Technol.,2017

3. Nonlinear mapping based impact angle control guidance with seeker's field-of-view constraint;Liu;Aerosp. Sci. Technol.,2019

4. New design methodology for impact angle control guidance for various missile and target motions;Seo;IEEE Trans. Control Syst. Technol.,2018

5. Three-dimensional guidance for various target motions with terminal angle constraints using twisting control;Hu;IEEE Trans. Ind. Electron.,2019

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