Nonlinear Autopilot Design for Endo- and Exoatmospheric Interceptor With Thrust Vector Control-Reference-Cited by-同舟云学术

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Nonlinear Autopilot Design for Endo- and Exoatmospheric Interceptor With Thrust Vector Control

Published:2020-02 Issue:1 Volume:56 Page:796-810
ISSN:0018-9251
Container-title:IEEE Transactions on Aerospace and Electronic Systems
language:
Short-container-title:IEEE Trans. Aerosp. Electron. Syst.

Author:

Hong Ju-Hyeon^ORCID,Lee Chang-Hun^ORCID

Publisher

Institute of Electrical and Electronics Engineers (IEEE)

Subject

Electrical and Electronic Engineering,Aerospace Engineering

Link

http://xplorestaging.ieee.org/ielx7/7/8986737/08731909.pdf?arnumber=8731909

Cited by 5 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. Optimal Control Approach to Design a Three-Loop Autopilot for a Tactical Missile;Unmanned Systems;2024-04-03

2. Control Allocation for Spin Interceptor with Aerodynamics and Lateral Thrust Blended;Springer Aerospace Technology;2024

3. Robust gain-scheduled missile autopilot design based on multifrequency extended state observers;Chinese Journal of Aeronautics;2023-12

4. An Adaptive Sliding Mode Compound Control Method of Interceptors;Lecture Notes in Electrical Engineering;2023

5. Control Allocation Strategies for a Hybrid Controlled Missile with NDI Autopilot;2022 13th Asian Control Conference (ASCC);2022-05-04

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