Title:
ATTITUDE CONTROL DEVICE
Document Type and Number:
Japanese Patent JP2023121989
Kind Code:
A
Abstract:
To provide an attitude control device that can stabilize an attitude of a fuselage quickly.SOLUTION: A rotor control device 50 that controls an attitude of a fuselage of an aircraft comprises a VTOL rotor control unit 76 that controls respective rotors, on the basis of a roll moment command value, a pitch moment command value and a yaw moment command value. When magnitude of the roll moment value or magnitude of the pitch moment command value is equal to or greater than a threshold, the VTOL rotor control unit 76 controls respective rotors without using the yaw moment command value.SELECTED DRAWING: Figure 4
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Inventors:
TSUJIMOTO RYUTA
Application Number:
JP2022025390A
Publication Date:
September 01, 2023
Filing Date:
February 22, 2022
Export Citation:
Assignee:
HONDA MOTOR CO LTD
International Classes:
B64C13/18; B64C27/08
Attorney, Agent or Firm:
Takehiro Chiba
Toshiyuki Miyadera
Takayuki Chima
Yasuharu Nakasone
Shiro Sakai
Tosuke Sekiguchi
Toshiyuki Miyadera
Takayuki Chima
Yasuharu Nakasone
Shiro Sakai
Tosuke Sekiguchi
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