Pulse Motor Optimization via Mission Charts for an Exoatmospheric Interceptor

Author:

Phillips Craig A.1,Malyevac D. Stephen1

Affiliation:

1. U.S. Naval Surface Warfare Center, Dahlgren, Virginia 22448

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

Cited by 8 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Singular-Perturbation-based Intelligent Midcourse Guidance for Air-to-Air Missiles Equipped with Dual-Pulse Motor;2023 14th International Conference on Mechanical and Aerospace Engineering (ICMAE);2023-07-18

2. Finite-time composite guidance law with input constraint and dynamics compensation;Chinese Journal of Aeronautics;2020-02

3. Extended state observer-based finite-time guidance laws on account of thruster dynamics;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2019-02-12

4. Design and experimental studies on ceramic port cover for dual pulse motor;Acta Astronautica;2011-06

5. Model Predictive Lateral Pulse Jet Control of an Atmospheric Rocket;Journal of Guidance, Control, and Dynamics;2002-09

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