کد مقاله | کد نشریه | سال انتشار | مقاله انگلیسی | نسخه تمام متن |
---|---|---|---|---|
5004676 | 1461201 | 2015 | 15 صفحه PDF | دانلود رایگان |
- 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.
Journal: ISA Transactions - Volume 54, January 2015, Pages 60-74