Title:
AIRCRAFT BODY WITH PROPELLER, CONTROL METHOD THEREOF, AND PROGRAM
Document Type and Number:
Japanese Patent JP2023125306
Kind Code:
A
Abstract:
To provide an aircraft body with a propeller, a control method thereof, and a program that can improve controllability even when a propeller cover is arranged to surround the radial outside of the propeller of the aircraft body with the propeller in order to improve quietness.SOLUTION: A drone 60 comprises: a controller 120 that determines a control amount for flight control according to an instruction from the outside; a drive unit 150 that rotates a propeller 610 according to an operation amount; an operation unit 140 that determines the operation amount according to the control amount; and a measurement unit 160 that detects that the drone 60 has come into a state corresponding to the instruction. In the drone 60, the propeller 610 is controlled on the basis of a differential response delay between a first response delay time calculated in a state with no propeller cover attached and a second response delay time calculated in a state with the propeller cover attached, where the response delay time is a differential between a first time point when the operation unit 140 determined the operation amount and a second time point when the measurement unit 160 performed the detection.SELECTED DRAWING: Figure 1
Inventors:
SHINDO HIROTAKA
Application Number:
JP2022029317A
Publication Date:
September 07, 2023
Filing Date:
February 28, 2022
Export Citation:
Assignee:
CANON KK
International Classes:
B64C13/04; B64C27/08; B64C39/02
Attorney, Agent or Firm:
Betsuyaku Shigehisa