Abstract
This work presents a method for missile autopilot design in the presence of actuator and uncertain dynamics. Nonlinear control algorithms are derived based on both missile aerodynamics and actuator dynamics. To account for system nonlinearities and uncertainties due to varying flight conditions, a memory-based compensation unit is developed and integrated into the strategy. Simulation on EMRAAT missile validates the effectiveness of the proposed control method.
| Original language | English |
|---|---|
| Title of host publication | Acquisition, Tracking, and Pointing XIV |
| Editors | Michael K. MASTEN, Larry A. STOCKUM |
| Publisher | SPIE |
| Pages | 111-122 |
| Number of pages | 12 |
| DOIs | |
| Publication status | Published - Jul 2000 |
| Externally published | Yes |
| Event | Aerosense 2000 - Orlando, United States Duration: 24 Apr 2000 → 28 Apr 2000 |
Conference
| Conference | Aerosense 2000 |
|---|---|
| Country/Territory | United States |
| City | Orlando |
| Period | 24/04/00 → 28/04/00 |
Funding
This work was partially supported by Air Force Office of Scientific Research (AFOSR) under subcontract F49620-98-0441.
Keywords
- Actuator dynamics
- autopilot
- missile control
- nonlinear system
- trajectory tracking
- stability