Bounded Differential Game Guidance Law for Interceptor Missiles with Aero Fins and Reaction Jets
Author:
Publisher
Japan Society for Aeronautical and Space Sciences
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://www.jstage.jst.go.jp/article/tjsass/53/182/53_182_275/_pdf
Reference14 articles.
1. 1) Hirokawa, R., Sato, K. and Manabe, S.: Autopilot Design for a Missile with Reaction-Jet Using Coefficient Diagram Method, AIAA Guidance, Navigation, and Control Conference and Exhibit, Montreal, Canada, August 2001.
2. Missile Controlled by Lift and Divert Thrusters Using Nonlinear Dynamic Sliding Manifolds
3. Quantized Control Allocation of Reaction Control Jets and Aerodynamic Control Surfaces
4. New Interceptor Guidance Law Integrating Time-Varying and Estimation-Delay Models
5. Comparison of Optimal Control and Differential Game Intercept Missile Guidance Laws
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