Journal of Projectiles, Rockets, Missiles and Guidance >
An Approach of Lateral Static Unstable Missile's Angle of Attack Boundary Analysis
Received date: 2009-04-10
Online published: 2025-05-28
During initial phase of engineering design, control system designers should analyze pneumatic features to quickly judge if guidance and control system performance can meet the requirements. Based on some kinds of raw control structure, in the paper, the influences of lateral static stabilization were analyzed, and calculation method of the maximum stable range was given. Its physical concept is clear and easy to calculate. The simulation result shows the flight angle of attack boundary value can be used for evaluating aerodynamic outline and estimating the guidance and control system's performance.
Key words： autopilot; channels coupling; lateral static instability; space stability
LI Younian , CHEN Xingyang , YANG Yurong . An Approach of Lateral Static Unstable Missile's Angle of Attack Boundary Analysis[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2010 , 30(2) : 1 -3,70 . DOI: 10.15892/j.cnki.djzdxb.2010.02.067
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