Abstract
In order to avoid cross couplings between the vertical and lateral motion, decoupling control of a double-channel control rolling missile autopilot was studied. Such couplings in autopilot loop are analyzed. Couplings of motion, control and the accelerometer placed a distance ahead of the c. g. exist in the rolling missile autopilot loop. Test results showed that the autopilot design needs decoupling. Trajectory simulation was conducted for a certain kind of missile controlled under optimization command. Simulation results proved that the scheme was feasible and had perfect application value.
| Original language | English |
|---|---|
| Pages (from-to) | 11-14 |
| Number of pages | 4 |
| Journal | Beijing Ligong Daxue Xuebao/Transaction of Beijing Institute of Technology |
| Volume | 28 |
| Issue number | 1 |
| Publication status | Published - Jan 2008 |
Keywords
- Autopilot
- Coupling
- Decoupling
- Double-channel
- Rolling missile
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Chen, L. J., Liu, L., & Yu, J. Q. (2008). Decoupling control of a double-channel control rolling missile autopilot. Beijing Ligong Daxue Xuebao/Transaction of Beijing Institute of Technology, 28(1), 11-14.