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Coning motion instability of spinning missiles induced by hinge moment

  • Published:2013-10 Issue:1 Volume:30 Page:239-245
  • ISSN:1270-9638
  • Container-title:Aerospace Science and Technology
  • language:en
  • Short-container-title:Aerospace Science and Technology

Author:

Zhou Wei,Yang Shuxing,Dong Jinlong

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference22 articles.

1. Ballistics: Theory and Design of Guns and Ammunition;Carlucci,2007

2. Flight stability of an asymmetric projectile with activating canards;Cooper;Journal of Spacecraft and Rockets,2012

3. Guided Weapon Control Systems;Garnell,1980

4. Stability of spinning missiles with an acceleration autopilot;Li;Journal of Guidance, Control, and Dynamics,2012

5. Modern Exterior Ballistics;McCoy,1999

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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. Controller design and stability analysis for spinning missiles via tensor product;Aerospace Science and Technology;2022-11

3. Generalized Control Coupling Effect of Spinning Guided Projectiles;IEEE Transactions on Aerospace and Electronic Systems;2022-10

4. Vibration Suppression of Electromechanical Actuator Considering Backlash Nonlinearity;Journal of Physics: Conference Series;2022-10-01

5. Stability of Spinning Missiles Guided by Trajectory Tracking Guidance Law;2022 34th Chinese Control and Decision Conference (CCDC);2022-08-15
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