A trajectory shaping guidance law with field-of-view angle constraint and terminal limits
Author:
Affiliation:
1. School of Mechatronical Engineering, Beijing Institute of Technology,Beijing,China,100081
2. Beijing Aerospace Technology Institute,Beijing,China,100074
3. School of Aerospace Engineering, Beijing Institute of Technology,Beijing,China,100081
Publisher
Institute of Electrical and Electronics Engineers (IEEE)
Subject
General Earth and Planetary Sciences,General Environmental Science
Link
http://xplorestaging.ieee.org/ielx7/5971804/9775056/09775051.pdf?arnumber=9775051
Reference30 articles.
1. Near optimal midcourse guidance law for flight vehicle
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3. Sliding-Mode Guidance and Control for All-Aspect Interceptors with Terminal Angle Constraints
4. A Nonlinear Suboptimal Guidance Law with 3D Impact Angle Constraints for Ground Targets
5. Tactical and Strategic Missile Guidance, Sixth Edition
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