Article ID Journal Published Year Pages File Type
5004676 ISA Transactions 2015 15 Pages PDF
Abstract

•A novel filter is proposed to estimate the velocity in sense of finite time.•A novel finite-time output feedback relative position coordinated controller is developed.•Simulation results validate the effectiveness and feasibility.

This paper investigates finite-time relative position coordinated tracking problem by output feedback for spacecraft formation flying without velocity measurement. By employing homogeneous system theory, a finite-time relative position coordinated tracking controller by state feedback is firstly developed, where the desired time-varying trajectory given in advance can be tracked by the formation. Then, to address the problem of lack of velocity measurements, a finite-time output feedback controller is proposed by involving a novel filter to recover unknown velocity information in a finite time. Rigorous proof shows that the proposed control law ensures global stability and guarantees the position of spacecraft formation to track a time-varying reference in finite time. Finally, simulation results are presented to illustrate the performance of the proposed controller.

Related Topics
Physical Sciences and Engineering Engineering Control and Systems Engineering
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