Optimization of three-loop missile autopilot gain under crossover frequency constraint-Reference-Cited by-同舟云学术

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Optimization of three-loop missile autopilot gain under crossover frequency constraint

Published:2016-02 Issue:1 Volume:12 Page:32-38
ISSN:2214-9147
Container-title:Defence Technology
language:en
Short-container-title:Defence Technology

Author:

Abd-elatif M.A.^ORCID,Qian Long-jun,Bo Yu-ming

Publisher

Elsevier BV

Subject

Metals and Alloys,Mechanical Engineering,Ceramics and Composites,Computational Mechanics

Reference16 articles.

1. Why modern controllers can go unstable in practice;Nesline;J Guid Control Dyn,1984

2. Overview of missile flight control systems;Jackson;Johns Hopkins APL Tech Dig,2010

3. Tactical and strategic missile guidance;Zarchan,2002

4. Analysis and improvement of missile three-loop autopilots;De-fu;J Syst Eng Electron,2009

5. An analytical design method for the missile two-loop acceleration autopilot;Hui,2012

Cited by 9 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. Missile Guidance using Proportional Navigation and Machine Learning;Journal of Engineering Research and Sciences;2024-03

3. Design Methodology of a Mini-Missile Considering Flight Performance and Guidance Precision;Journal of Systems Engineering and Electronics;2024-02

4. Bilinear Interpolation of Three–Dimensional Gain–Scheduled Autopilots;Sensors;2023-12-19

5. Gain-scheduled h₂/h_∞ autopilot design with regional pole placement constraints: An LMI-based approach;SCI IRAN;2021

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