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EFFECT ON BALLISTIC CHARACTERISTICS OF FINNED ROCKET DUE TO SURFACE WIND AND ITS CORRECTION

机译:表面风引起的翅片火箭弹道特性的影响及其校正

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In this paper, the effect on ballistic characteristics of a finned rocket due to surface wind is studied in the complex plane. The angle of attack equation is established including the cross motion and roll equation. The ballistic characteristics of the parameters such as θ , ψ , δ_(r1), δ_(r2), ?_α, ?_2,γ, X and Z are simulated and analyzed. The simulation results show that the surface wind would arouse sizeable scatter at the initial trajectory because of the low flight velocity and surface wind field. A correction method is advanced to decrease the dispersion of the finned rocket by using the energy and aerodynamic control method, and the correction formulas are given to increase the firing accuracy.
机译:在本文中,在复杂平面中研究了由表面风引起的翅片火箭的弹道特性的影响。建立攻击方程角度,包括横向运动和滚动方程。模拟并分析了诸如θ,ψ,Δ_(R1),Δ_(R2),Δ_α,Δ_2,γ,x和z的参数的弹道特性。仿真结果表明,由于飞行速度和表面风场,表面风将在初始轨迹处引起大幅度散射。通过使用能量和空气动力学控制方法,提前校正方法以减小翅片火箭的分散,并且校正公式被赋予燃烧精度。

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