Command filtered back-stepping missile integrated guidance and autopilot based on extended state observer
This article focuses on the missile integrated guidance and autopilot design in the end-game phase with control input saturation. First, the nonlinear integrated guidance and autopilot model is developed with third actuator dynamics, where the control surface deflection has magnitude constraint. Sec...
| Main Authors: | , , , , |
|---|---|
| Format: | Article |
| Language: | English |
| Published: |
SAGE Publishing
2017-11-01
|
| Series: | Advances in Mechanical Engineering |
| Online Access: | https://doi.org/10.1177/1687814017733251 |