Coupling analysis and dynamic stability boundary of spinning missiles considering actuator dynamics and autopilot
Author:
Funder
National Natural Science Foundation of China
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference30 articles.
1. Dynamic modeling and stability analysis of a flexible spinning missile under thrust;Xu;Int. J. Mech. Sci.,2016
2. Coning motion stability of spinning missiles with strapdown seekers;He;Aeronaut. J.,2016
3. Dynamic stability of rolling missiles employing a two-loop autopilot with consideration for the radome aberration parasitic feedback loop;Zheng;Aerosp. Sci. Technol.,2017
4. Dynamic stability of rolling missiles with angle-of-attack feedback three-loop autopilot considering parasitic effect;Tian;Aerosp. Sci. Technol.,2017
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3. Generalized Control Coupling Effect of Spinning Guided Projectiles;IEEE Transactions on Aerospace and Electronic Systems;2022-10
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