Abstract
In this paper, a robust multi-objective design for the control of a launcher during atmospheric flight is investigated. This approach is based on the Cross Standard Form formulation which allows to incorporate the various specifications of the launcher problem in a streamlined manner. An important feature of this approach is that a non-conventional LQG/LTR approach, required to satisfy time-domain specifications, can be embedded into a more general standard problem in order to account for frequency-domain robustness constraints. The specific form of this standard problem is also very interesting for gain scheduling.
Original language | English |
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Pages (from-to) | 1243-1252 |
Number of pages | 10 |
Journal | Control Engineering Practice |
Volume | 11 |
Issue number | 11 |
DOIs | |
Publication status | Published - Nov 2003 |
Externally published | Yes |
Keywords
- Cross standard form
- Gain scheduling
- Launcher
- Multi-objective design
- Robustness