Command filtered back-stepping missile integrated guidance and autopilot based on extended state observer
Author:
Affiliation:
1. National University of Defense Technology, Changsha, China
Publisher
SAGE Publications
Subject
Mechanical Engineering
Link
http://journals.sagepub.com/doi/pdf/10.1177/1687814017733251
Reference30 articles.
1. Integrated Guidance and Control of Missiles With$theta hbox - D$Method
2. Numerical State-Dependent Riccati Equation Approach for Missile Integrated Guidance Control
3. Sliding-Mode Control for Integrated Missile Autopilot Guidance
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