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Terminal Sliding Mode Control for Spatial Descent of a Stratospheric Airship*

机译:平流层飞艇空间下降的终端滑模控制*

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摘要

Addressing the problem of spatial descending control with wind disturbance, this paper presents a spatial path following controller of the stratospheric airship based on the theories of three-dimensional vector field guidance and terminal sliding mode control. Firstly, the nonlinear under-actuated stratospheric airship model is presented. Secondly, the three-dimensional vector field guidance law is designed to calculate real-time desired attitudes of the stratospheric airship for the purpose of guiding the stratospheric airship to follow the desired path. Thirdly, the terminal sliding mode controller is designed to control the airship to follow the desired attitudes. Finally, simulation results validate the effectiveness of the proposed controller.
机译:针对空间扰动引起的空间下降控制问题,本文基于三维矢量场制导和终端滑模控制理论,提出了一种平流层飞艇控制器的空间路径跟踪方法。首先,提出了非线性欠驱动平流层飞艇模型。其次,设计了三维矢量场制导律,以计算平流层飞艇的实时期望姿态,以引导平流层飞艇遵循期望的路径。第三,终端滑模控制器被设计成控制飞艇遵循期望的姿态。最后,仿真结果验证了所提出控制器的有效性。

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