用广义哈密顿公式设计导弹自动驾驶仪

Proceedings. The First IEEE Regional Conference on Aerospace Control Systems, Pub Date : 1993-05-25 DOI:10.1109/AEROCS.1993.721027

Ching-Fang Lin, J. Cloutier, J. Evers

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引用次数: 4

摘要

介绍了鲁棒多变量控制在导弹自动驾驶仪设计中的应用。将一种基于广义哈密顿公式的协同算法应用于DASH II导弹系统的鲁棒自动驾驶仪设计。该设计承受了显著的运动和惯性耦合、气动参数变化和高频柔性效应。

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Missile Autopilot Design Using a Generalized Hamiltonian Formulation

This paper presents the application of robust multivariable control to a missile autopilot design. A synergistic algorithm based on the generalized Hamiltonian formulation is applied to robust autopilot design for the HAVE DASH II missile system. The design endures significant kinematic and inertia couplings, aerodynamic parameter variations and high frequency flexible effects.

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Proceedings. The First IEEE Regional Conference on Aerospace Control Systems,

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