Author:
Zhang Long,Zhang Yan,Li Rui,Wang Hai
Abstract
Abstract
Aiming at the rapid manoeuvring launching requirements of anti-aircraft guided projectiles, the flight stability analysis of a guided projectile launch is carried out, and the initial disturbance parameters model based on equivalent analysis is established. The initial disturbance parameters model and the guided projectile rigid body trajectory model are combined. The relationship between the dynamics and kinematics of the guided projectile is described. The flight performance of the guided projectile is analysed by the stability theory and the criterion. The influence of the launch disturbance on the flight stability is obtained, and the allowed boundary of the guided projectile launch is determined.
Subject
General Physics and Astronomy
Cited by
1 articles.
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