Instability of Spinning Projectiles During Terminal Guidance

Author:

Lloyd K.H.,Brown D.P.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

General Engineering

Cited by 28 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. 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. A novel quasi-dynamic guidance law for a dynamic dual-spin projectile with non-conventional, asymmetric roll constraints;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2022-03-01

3. Research on Instability Boundaries of Control Force for Trajectory Correction Projectiles;Mathematical Problems in Engineering;2019-03-11

4. Dynamic Response Analysis for a Terminal Guided Projectile With a Trajectory Correction Fuze;IEEE Access;2019

5. Homotopy-Analysis-Method-Based Solutions of Quintic Nonlinear Angular Motion for Projectiles;Journal of Spacecraft and Rockets;2018-05

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