Abstract
This paper investigates the problem of finite-time velocity-free autonomous rendezvous for spacecraft in the presence of external disturbances during the terminal phase. First of all, to address the problem of lack of relative velocity measurement, a robust observer is proposed to estimate the unknown relative velocity information in a finite time. It is shown that the effect of external disturbances on the estimation precision can be suppressed to a relatively low level. With the reconstructed velocity information, a finite-time output feedback control law is then formulated to stabilize the rendezvous system. Theoretical analysis and rigorous proof show that the relative position and its rate can converge to a small compacted region in finite time. Numerical simulations are performed to evaluate the performance of the proposed approach in the presence of external disturbances and actuator faults.
| Original language | English |
|---|---|
| Pages (from-to) | 52-60 |
| Number of pages | 9 |
| Journal | Acta Astronautica |
| Volume | 144 |
| DOIs | |
| Publication status | Published - Mar 2018 |
Keywords
- Actuator faults
- External disturbances
- Finite-time convergence
- Spacecraft rendezvous
- Velocity-free
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