Optimal Fixed-Interval Integrated Guidance-Control Laws for Hit-to-Kill Missiles

Author:

Menon P.1,Sweriduk Gregory1,Ohlmeyer Ernest2

Affiliation:

1. Optimal Synthesis Inc.

2. Naval Surface Warfare Center

Publisher

American Institute of Aeronautics and Astronautics

Cited by 15 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. Design of integrated Guidance and control system in the pitch channel using observer based chattering free sliding mode theory;Journal of Control;2020-05-01

2. Adaptive fin failures tolerant integrated guidance and control based on backstepping sliding mode;Transactions of the Institute of Measurement and Control;2020-01-10

3. Optimal Error Dynamics in Missile Guidance;Optimal Guidance and Its Applications in Missiles and UAVs;2020

4. Interdependent Estimation and Guidance With Zero-Effort-Miss Enforcement;IEEE Transactions on Aerospace and Electronic Systems;2019-08

5. A New Collision Control Guidance Law Based on Speed Control for Kill Vehicles;International Journal of Aeronautical and Space Sciences;2019-02-05

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