Stability of Spinning Missiles Guided by Trajectory Tracking Guidance Law

Trajectory tracking guidance is employed widely by low cost missiles for the characteristic of easy to implement. However, for spinning missile, the guidance loop may result in dynamic unstable in the form of a divergent coning motion. Due to the cross-coupling effects between the pitch and yaw chan...

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Vydané v:	Chinese Control and Decision Conference s. 4503 - 4509
Hlavní autori:	Zhou, Zhiming, Liu, Zhen
Médium:	Konferenčný príspevok..
Jazyk:	English
Vydavateľské údaje:	IEEE 15.08.2022
Predmet:	Acceleration autopilot Actuators Missiles Numerical simulation Simulation Spinning missile Stability Stability criteria Stability criterions Tracking loops Trajectory tracking Trajectory tracking guidance
ISSN:	1948-9447
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