Three dimensional impact angle constrained integrated guidance and control for missiles with input saturation and actuator failure

Author:

Wang Weihong,Xiong Shaofeng,Wang Sen,Song Siyang,Lai Chao

Funder

National Defense Pre-Research Foundation of China

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference49 articles.

1. Integrated guidance and control for homing missiles;Palumbo;Johns Hopkins APL Techn. Digest,2004

2. Partial integrated guidance and control for missiles with three-dimensional impact angle constraints;Wang;J. Guid. Control Dyn.,2014

3. Integrated design of agile missile guidance and autopilot systems;Menon;Control Eng. Pract.,2001

4. Design of an integrated strapdown guidance and control system for a tactical missile;Williams,1983

5. Integrated estimation, guidance, and control system design using game theoretic approach;Lin,1992

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