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首页> 外文期刊>Acta astronautica >Robust adaptive position and attitude-tracking controller for satellite proximity operations
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Robust adaptive position and attitude-tracking controller for satellite proximity operations

机译:用于卫星近场操作的鲁棒自适应位置和姿态跟踪控制器

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摘要

This paper studies the pose tracking control problem for satellite proximity operations between a target and a chaser satellite, by which we mean that the chaser is required to track a desired time-varying trajectory given in advance with respect to the target. Firstly, by consulting an adaptive sliding-mode control method in literature developed for a class of nonlinear uncertain systems, an effective pose tracking controller is obtained. This controller requires no information about the mass and inertia matrix of the chaser, and takes into account the gravitational acceleration, the gravity-gradient torque, the J(2) perturbing acceleration, and unknown bounded disturbance forces and torques. Then, an updated controller is proposed by combining the aforementioned controller and the unscented Kalman filter (UKF). This updated controller estimates the inertial parameters of the chaser through UKF, so it is of better adaptive ability to the initial estimation of the inertial parameters. Finally, numerical simulations are given to demonstrate the effectiveness of the proposed controllers. The simulation results show that the updated controller is more accurate.
机译:本文研究了目标与追赶者卫星之间的卫星接近操作的姿态跟踪控制问题,这意味着我们需要追赶者追踪相对于目标事先给出的所需时变轨迹。首先,通过参考针对一类非线性不确定系统开发的文献中的自适应滑模控制方法,获得了一种有效的姿态跟踪控制器。该控制器不需要有关追赶者的质量和惯性矩阵的信息,并考虑了重力加速度,重力梯度转矩,J(2)扰动加速度以及未知的有界干扰力和转矩。然后,通过组合前述控制器和无味卡尔曼滤波器(UKF)来提出更新的控制器。该更新的控制器通过UKF估算了追赶者的惯性参数,因此对惯性参数的初始估算具有更好的自适应能力。最后,通过数值仿真证明了所提出控制器的有效性。仿真结果表明,更新后的控制器更加准确。

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