Nonlinear control of aerial vehicles subjected to aerodynamic forces

D. Pucci, T. Hamel, P. Morin, C. Samson
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引用次数: 16

Abstract

The paper contributes towards the development of a unified control approach for longitudinal aircraft dynamics. It states conditions that allow to adapt the control strategies developed for orientation-independent external forces to the orientation-dependent case. The control strategy presented here is a step to the automatic monitoring of the flight transitions between hovering and cruising for convertible aerial vehicles.
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飞行器在空气动力作用下的非线性控制
本文为建立统一的飞机纵向动力学控制方法做出了贡献。它说明了允许将针对与方向无关的外力开发的控制策略适应于与方向相关的情况的条件。本文提出的控制策略是实现可转换飞行器悬停与巡航飞行过渡自动监控的一个步骤。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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