In this paper, a flexible spacecraft attitude control scheme that guarantees vibration suppression and prescribed performance on transient-state behavior is proposed. Here, parametric uncertainty, external disturbance...In this paper, a flexible spacecraft attitude control scheme that guarantees vibration suppression and prescribed performance on transient-state behavior is proposed. Here, parametric uncertainty, external disturbance, unmeasured elastic vibration, actuator saturation, and even configuration misalignment are considered. To guarantee prescribed performance bounds on the transient-and steady-state control errors, a performance constrained control law is formulated with an error transformed function. An elastic modal observer is employed to estimate the unmeasured flexible modal variables, and a command filter is adopted to avoid the tedious analytical computations of time derivatives of virtual control inherent in the control design. Subsequently, a novel auxiliary system is developed to compensate the adverse effects of the actuator saturation constraints, and a compensation term is integrated into the control law to tackle the configuration misalignment. A comparative simulation study is carried out to illustrate the effectiveness and advantages of the proposed approach.展开更多
根据结构控制系统的特点,提出了结构控制系统模态能控度的概念,进而提出了对各解耦子空间状态向量的规范化处理,并给出了规范化因子的计算公式。在此基础上,得到模态恢复区域任一方向上边界点向量的解析表达式。由此求出的模态恢复区域...根据结构控制系统的特点,提出了结构控制系统模态能控度的概念,进而提出了对各解耦子空间状态向量的规范化处理,并给出了规范化因子的计算公式。在此基础上,得到模态恢复区域任一方向上边界点向量的解析表达式。由此求出的模态恢复区域、模态能控度,是其真值的最佳逼近值。因此,本文发展和改进了Viswanathan C N 等提出的能控度概念及其计算方法,为应用能控度准则判断结构控制系统作动器配置方案的优劣,提供了一个可靠的工具。本文给出一个颤振主动抑制系统不同控制面配置方案模态能控度计算、比较的算例。展开更多
基金supported by the National Natural Science Foundation of China (Nos. 61703228 and 61673239)
文摘In this paper, a flexible spacecraft attitude control scheme that guarantees vibration suppression and prescribed performance on transient-state behavior is proposed. Here, parametric uncertainty, external disturbance, unmeasured elastic vibration, actuator saturation, and even configuration misalignment are considered. To guarantee prescribed performance bounds on the transient-and steady-state control errors, a performance constrained control law is formulated with an error transformed function. An elastic modal observer is employed to estimate the unmeasured flexible modal variables, and a command filter is adopted to avoid the tedious analytical computations of time derivatives of virtual control inherent in the control design. Subsequently, a novel auxiliary system is developed to compensate the adverse effects of the actuator saturation constraints, and a compensation term is integrated into the control law to tackle the configuration misalignment. A comparative simulation study is carried out to illustrate the effectiveness and advantages of the proposed approach.
文摘根据结构控制系统的特点,提出了结构控制系统模态能控度的概念,进而提出了对各解耦子空间状态向量的规范化处理,并给出了规范化因子的计算公式。在此基础上,得到模态恢复区域任一方向上边界点向量的解析表达式。由此求出的模态恢复区域、模态能控度,是其真值的最佳逼近值。因此,本文发展和改进了Viswanathan C N 等提出的能控度概念及其计算方法,为应用能控度准则判断结构控制系统作动器配置方案的优劣,提供了一个可靠的工具。本文给出一个颤振主动抑制系统不同控制面配置方案模态能控度计算、比较的算例。
