Abstract

A method for determining the values of the attitude angles of an aerial vehicle (AV) is considered. For the proposed method, the initial data are the values of overloads in the body-fixed coordinate system and velocity projections in the Earth’s normal coordinate system. It is proposed, using the approaches of direct methods for finding the optimal control, to parametrize the pitch, roll, and yaw angles, and then find the values of the parameters based on the initial data. The resulting optimization problem can be solved using a population algorithm.

中文翻译：

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基于直线运动参数测量的飞行器角位置估计

摘要

考虑一种用于确定飞行器（AV）姿态角值的方法。对于所提出的方法，初始数据是身体固定坐标系中的过载值和地球法向坐标系中的速度投影。提出使用直接方法寻找最优控制的方法，对俯仰角、横滚角和偏航角进行参数化，然后根据初始数据求出参数值。由此产生的优化问题可以使用总体算法来解决。