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Dynamical reduction and output-tracking control of the Lunar Exploration Light Rover (LELR)
- Source :
- 2016 IEEE Aerospace Conference.
- Publication Year :
- 2016
- Publisher :
- IEEE, 2016.
-
Abstract
- This paper presents the dynamical reduction and feedback linearization of the Lunar Exploration Light Rover to design an output-tracking torque controller for such a system. The rover is dynamically modeled as a system of rigid bodies that could be considered as a symmetric mechanical system. Its dynamical equations are reduced using the Chaplygin reduction of nonholonomic systems. The reduced dynamical system only involves the rotation and steering angles of the port front wheel. The steering angle and the travelled distance of the vehicle are considered the outputs of the resulting control system. Feedback linearization in the reduced phase space is then employed to derive a proportional-integral-derivative feedback, feedforward torque controller for the rover. Finally, a series of simulation studies are provided to show the robustness of the resulting controller under uncertainties of the dynamical parameters and the disturbance force in the form of friction at the rear wheels.
- Subjects :
- Nonholonomic system
0209 industrial biotechnology
Engineering
business.industry
Feed forward
Control engineering
02 engineering and technology
01 natural sciences
Computer Science::Robotics
Mechanical system
020901 industrial engineering & automation
Control theory
Robustness (computer science)
Control system
Phase space
0103 physical sciences
Feedback linearization
business
010301 acoustics
Equations for a falling body
Subjects
Details
- Database :
- OpenAIRE
- Journal :
- 2016 IEEE Aerospace Conference
- Accession number :
- edsair.doi...........bf54304436e3fb9db56340a12f8863ec
- Full Text :
- https://doi.org/10.1109/aero.2016.7500577