In the process of unmanned helicopter landing, when gears are touching down, rotation speed of main rotor and collective will both stay at high level, which threatens landing safety severely. This paper proposes a control design aimed at the situation, and then make a proof and simulation.
On safe landing control technology of unmanned helicopter
2016-08-01
370498 byte
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
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