文章给出了航天员的相对位置控制策略，并将全系数自适应控制和PID控制方法用于追踪器的姿态控制。
The relative position control strategy and method of the pilot are proposed. The all-coefficient adaptive control and PID control method are applied to the relative attitude control.
设定与指定之控制项相关联的工具提示文字，然后在指定的相对位置并于指定的持续期限内显示工具提示。
Sets the ToolTip text associated with the specified control, and then displays the ToolTip for the specified duration at the specified relative position.
考虑控制输入耦合，建立服务航天器对目标航天器的相对位置和姿态一体化耦合动力学模型。
Considering coupled control inputs, an integrated coupling relative position and attitude dynamic model of the on-orbit servicing spacecraft is built with respect to the target spacecraft.
应用推荐