Nonsingular Terminal Sliding Mode Guidance with Impact Angle Constraints
Author:
Affiliation:
1. Guidance, Control, and Decision Systems Laboratory, Department of Aerospace Engineering, Indian Institute of Science, Bangalore 560012, India
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
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.62737
Reference36 articles.
1. Sliding Mode Control in Electro-Mechanical Systems
2. Sliding-Mode Guidance and Control for All-Aspect Interceptors with Terminal Angle Constraints
3. Finite-time convergent guidance law with impact angle constraint based on sliding-mode control
4. Guidance Laws with Finite Time Convergence
5. Design and Simulation of Guidance Law with Angular Constraint Based on Non-singular Terminal Sliding Mode
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