Abstract
The H∞ control problem was proposed in the BTT autopilot design, among which the selection of the weight function and the establishment of the mode were the main focus. Firstly the ideal mathematical model of BTT missile was established in pitch, yaw-roll coupled form. According to the design demand the weight functions were selected and the augmented model was built up. Then the pitch and lateral autopilot were designed using H∞ theory.
| Original language | English |
|---|---|
| Pages (from-to) | 991-995 |
| Number of pages | 5 |
| Journal | Xitong Fangzhen Xuebao / Journal of System Simulation |
| Volume | 22 |
| Issue number | 4 |
| Publication status | Published - Apr 2010 |
Keywords
- Autopilot
- BTT
- BTT missile
- H theory