Aircraft control method and aircraft
A control method and technology of a flight control system, which are applied to the aircraft control method and the aircraft field, can solve the problems of small yaw control torque, increased FCS control pressure, video freeze, etc., and achieve high-precision control, ensure high quality, and solve problems. Video freeze effect
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Embodiment 1
[0086] An embodiment of the present invention provides an aircraft control method, please refer to image 3 , is a schematic flowchart of an aircraft control method provided by an embodiment of the present invention. The aircraft control method is applied to an aircraft to control the yaw of the aircraft and increase the stability of aerial photography of the aircraft. The aircraft includes a flight control system for controlling the aircraft and a gimbal control system for controlling the gimbal, so as to achieve high-precision shooting. Wherein, the aircraft can be various types of aircraft, for example, figure 1 and figure 2 10 in the aircraft.
[0087] Please refer to image 3 , the aircraft control method includes but is not limited to the following steps:
[0088] Step 110: The gimbal control system acquires the yaw control command input to the aircraft and the attitude angle information output from the gimbal.
[0089] The yaw control command is the yaw control c...
Embodiment 2
[0137] The embodiment of the present invention also provides an aircraft, please refer to Figure 7 , is a structural block diagram of an aircraft 200 according to an embodiment of the present invention, the aircraft 200 includes a fuselage 210 , an arm 220 , a power unit 230 , a gimbal 240 , a flight control system 250 and a gimbal control system 260 . The arm 220 is connected to the fuselage 210, the power device 230 is installed on the arm 220, and is used to provide the flying power for the aircraft 200, and the gimbal 240 is installed on the aircraft In the body 210 , the flight control system 250 is disposed on the body 210 , and the gimbal control system 260 is used to control the gimbal 240 and is connected to the flight control system 250 in communication.
[0138] The pan-tilt control system 260 is used for: acquiring the yaw control command input to the aircraft 200 and the attitude angle information output by the pan-tilt 240; according to the yaw control command i...
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