With the industrialization of microcomputer technology and flight drive technology, small “X” quad-rotor UAV has been widely used as a typical model. But what follows is higher re quirements for performance and security. The static hovering po wer of general aerial small UAV is 200 to 300 watts and the flight altitude is more than 12 meters. Such a device is undoubtedly pot entially dangerous. The solution of these problems still depends o n the application of more reliable control rate. This paper analyz es the flight mechanism of “X” quad-rotor UAV in detail, and des igns and simulates the control system on this basis.
Research on adaptive control algorithm of small quad-rotor UAV based on sliding mode control
23.09.2021
1368268 byte
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Adaptive backstepping sliding mode trajectory tracking control for a quad-rotor
British Library Online Contents | 2012
|Reduced-Order Observer Based Sliding Mode Control for a Quad-Rotor Helicopter
British Library Online Contents | 2016
|Feedback linearization based sliding mode control system for quad-rotor UAV with a Ground effect
Europäisches Patentamt | 2021
Feedback linearization based sliding mode control system for quad-rotor UAV with a Ground effect
Europäisches Patentamt | 2020
|