Abstract
This paper addresses the robust control problem of spacecraft body-fixed hovering near a noncooperative target in the presence of parametric uncertainties and disturbances. A closed-form nonlinear robust H∞ controller constructed by the solution of Hamilton-Jacobi-Isaacs (HJI) inequality is designed, which can stabilize the closed-loop system with the H∞ performance. To obtain the solution of HJI, an effective numerical approximation approach called the modified θ-D method is proposed, which can obtain a numerical approximation solution of HJI by only solving one algebraic Riccati inequality and several Lyapunov equations rather than a partial differential inequality. The detailed numerical calculation processes of solving the HJI are presented, which shows that the modified θ-D method can be implemented offline with less computational burden. Finally, the effectiveness of the designed robust control scheme is demonstrated via a numerical example.
Original language | English |
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Article number | 8599001 |
Pages (from-to) | 2451-2463 |
Number of pages | 13 |
Journal | IEEE Transactions on Aerospace and Electronic Systems |
Volume | 55 |
Issue number | 5 |
DOIs | |
Publication status | Published - Oct 2019 |
Externally published | Yes |
Keywords
- H∞ performance
- modified θ-D method
- noncooperative target
- robust control
- spacecraft hovering