Hybrid Genetic Algorithm fuzzy rule based guidance and control for launch vehicle
Author:
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx5/6112291/6121619/06121651.pdf?arnumber=6121651
Cited by 6 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. On efficient matching of spatiotemporal rules;Future Generation Computer Systems;2023-09
2. State-of-the-Art Integrated Guidance and Control Systems in Unmanned Vehicles: A Review;IEEE Systems Journal;2021-09
3. Launch vehicle ascent flight attitude control using direct adaptive generalized dynamic inversion;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2018-11-28
4. ADAPTIVE FUZZY SLIDING MODE CONTROL: APPLICATION TO SATELLITE LAUNCH VEHICLE’S ATTITUDE CONTROL;Mechatronic Systems and Control (formerly Control and Intelligent Systems);2018
5. Robust launch vehicle’s generalized dynamic inversion attitude control;Aircraft Engineering and Aerospace Technology;2017-10-02
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