Near-eigenaxis rotation control law design for moving-to-rest maneuver

Adaptive fuzzy PD+ based spacecraft attitude maneuvering

“…，自适应控制[习， 鲁棒控制 [巧，滑模变结构 [ 4 ] ，神经网络 [5 ] 等控制方法运用到刚体航 天器姿态控制中。 但在实 际工程中考虑到航天器的成本和 发射风险，PD+控制以其设计简单易于实现等特点成为了 刚体航天器姿态机动控制系统的常用设计方法 [6 ] 。 PD+控制是由PD反馈和动态逆设计结合形成的 [ 7 ] 。 动态逆设计是利用全状态反馈来抵消系统中的非线性工页， 然后运用传统线性控制的方法来分析新系统 [ 8 ] 。 动态逆设 计简化了控制器增益系数的整定， 降低了控制器设计的难 度， 因此 PD+控制在近年来得到了广泛的研究 [9][10][11] 。 针 对刚体航天器 Rest-to-Rest机动和 Moving-to-Rest机动问 题， 文 [9 ] 和文 [ …”

Adaptive Fuzzy PD+ Control for Attitude Maneuver of Rigid Spacecraft

“…For the obtained system, conventional linear control techniques, such as the PD technique, can be applied to achieve the desired closed-loop system, which simplifies the design of the controller [8]. Consequently studied extensively in recent years [9][10][11][12][13][14][15][16]. A PD+ attitude control law of rigid spacecraft for rest-to-rest attitude maneuver and move-to-rest attitude maneuver were designed in [9,10], respectively.…”

“…Consequently studied extensively in recent years [9][10][11][12][13][14][15][16]. A PD+ attitude control law of rigid spacecraft for rest-to-rest attitude maneuver and move-to-rest attitude maneuver were designed in [9,10], respectively. In [11], the Matrosov theorem and Barbalat lemma were adopted to analyze the asymptotical stability of the PD+ attitude control system.…”

Attitude tracking control of on-orbit-servicing spacecraft based on eigenaxis maneuver

“…It has been widely reported that the eigenaxis rotation enables to attitude maneuver rapid completed in the shortest path and achieve the optimization of energy and time consumption [4][5][6][7][8][9][10]. Considering the differences of initial maneuver condition, these eigenaxis algorithms can be divided into rest-to-rest maneuver and move-torest maneuver.…”

“…Considering the differences of initial maneuver condition, these eigenaxis algorithms can be divided into rest-to-rest maneuver and move-torest maneuver. The former is usually used for the maneuver among different stable attitude modes [4][5][6][7], and the latter is used for initial attitude capture where the spacecraft is motion before maneuver [8][9][10].…”