Stability of Spinning Missiles with an Acceleration Autopilot-Reference-Cited by-同舟云学术

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Stability of Spinning Missiles with an Acceleration Autopilot

Published:2012-05 Issue:3 Volume:35 Page:774-786
ISSN:0731-5090
Container-title:Journal of Guidance, Control, and Dynamics
language:en
Short-container-title:Journal of Guidance, Control, and Dynamics

Author:

Li Keyong¹,Yang Shuxing¹,Zhao Liangyu¹

Affiliation:

1. Beijing Institute of Technology, 100081 Beijing, People’s Republic of China

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.56122

Reference21 articles.

1. Symmetric Missile Dynamic Instabilities

2. Ballistic Re-entry Vehicle Flight Dynamics

3. Angular motion of a re-entering symmetric missile

4. Missile and spacecraft coning instabilities

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1. Research on dynamic stability of rolling missiles employing direct/aerodynamic force compound control;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2024-05-02

2. Feedforward Compensation Enhanced Disturbance Rejection Control for a Spin-Stabilized Guided Projectile Subject to Actuator Rate Limit;Lecture Notes in Mechanical Engineering;2023-12-20

3. Observer-based robust high-order fully actuated attitude autopilot design for spinning glide-guided projectiles;Defence Technology;2023-11

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