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Control module of desaturation of the wheels, a device for controlling the attitude of a spacecraft and method of desaturation of the wheels associated

机译:车轮去饱和的控制模块,用于控制航天器姿态的装置以及相关的车轮去饱和的方法

摘要

This control module (22) of desaturation of the inertia wheels of an attitude control device (20) comprises a module of the actuation of the torques to be able to apply a spacecraft (10) in order to modify its orientation, is characterized in that it is capable of: - for each of the preceding passage, to estimate the gyroscopic torque the spacecraft (10) on the two orthogonal axes (xsat, zsat), and to estimate the disturbing torques applied to the spacecraft (10) on the two orthogonal axes (xsat, zsat); - for each current, to determine a first and second signals as a function of the gyroscopic torque and the estimated disturbing torques, and to apply the first and second signals to the system of the actuators to desaturate at least some of the inertia wheels when the spacecraft (10) is located in a portion of desaturation authorized.
机译:该姿态控制装置(20)的惯性轮去饱和的控制模块(22)包括用于致动扭矩的模块,该扭矩模块能够施加航天器(10)以改变其方向,其特征在于它能够:-对于每个先前的通过,在两个正交轴(xsat,zsat)上估计航天器(10)的陀螺转矩,并在两个正交轴上估计施加到航天器(10)的干扰转矩正交轴(xsat,zsat); -对于每个电流,确定作为陀螺仪扭矩和估计干扰扭矩的函数的第一和第二信号,并将第一和第二信号施加到致动器的系统上,以使至少一些惯性轮饱和。航天器(10)位于授权的脱饱和部分中。

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