Optimal control of aircraft landing gear state feedback based on magneto rheological damper
- Resource Type
- Conference
- Authors
- Fu, Li; Chen, Shuai; Bai, Xueshan; Wang, Junhua
- Source
- 2018 Chinese Control And Decision Conference (CCDC) Chinese Control And Decision Conference (CCDC), 2018. :6673-6676 Jun, 2018
- Subject
- General Topics for Engineers
Power, Energy and Industry Applications
Robotics and Control Systems
Signal Processing and Analysis
Gears
Optimal control
Magnetomechanical effects
Shock absorbers
Mathematical model
Aircraft
Atmospheric modeling
Aircraft landing gear
Magneto rheological damper
Optimum control
- Language
- ISSN
- 1948-9447
The landing gear cushion Controller is one of the important parts of the aircraft undercarriage, and its performance directly affects the safety of aircraft landing. the dynamics model of landing gear cushion system based on magneto rheological fluid is established. The optimal control algorithm based on state feedback is introduced and the optimal control algorithm based on state feedback is used to simulate the landing gear cushioning system in this work. The simulation results show that the optimal control based on state feedback can effectively absorb the impact load energy.