Actuator Constrained Trajectory Generation and Control for Variable-Pitch Quadrotors
Control and trajectory generation algorithms for a quadrotor helicopter with variable-pitch propellers are presented. The control law is not based on near-hover assumptions, allowing for large attitude deviations from hover. The trajectory generation algorithm ts a time-parametrized polynomial thr...
| Main Authors: | , |
|---|---|
| Other Authors: | |
| Format: | Article |
| Language: | en_US |
| Published: |
American Institute of Aeronautics and Astronautics
2013
|
| Online Access: | http://hdl.handle.net/1721.1/81435 https://orcid.org/0000-0001-8576-1930 https://orcid.org/0000-0003-0776-7901 |