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Multimodal fusion manipulator and design method for electric vertical take-off and landing tilt-wing aircraft

A technology of vertical take-off and landing, design method, applied in vertical take-off and landing aircraft, aircraft, rotorcraft and other directions, can solve the problem of insufficient adaptation of mission characteristics

Active Publication Date: 2022-07-15
BEIHANG UNIV
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  • Description
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  • Application Information

AI Technical Summary

Problems solved by technology

[0005] In view of this, the present invention provides a multi-mode fusion manipulator and design method for an electric vertical take-off and landing tilt-wing aircraft to solve the problem of the existing manipulator and the task characteristics of the electric vertical take-off and landing tilt-wing aircraft in the prior art. The problem of insufficient adaptability

Method used

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  • Multimodal fusion manipulator and design method for electric vertical take-off and landing tilt-wing aircraft
  • Multimodal fusion manipulator and design method for electric vertical take-off and landing tilt-wing aircraft
  • Multimodal fusion manipulator and design method for electric vertical take-off and landing tilt-wing aircraft

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Embodiment 1

[0067] Examples of control command parameters for electric vertical take-off and landing aircraft are shown in Table 1

[0068] Table 1 Example of control command parameters for electric vertical take-off and landing tilt-wing aircraft

[0069]

[0070] In the embodiment, the left joystick travels -10~0~10~50 (m / s) in the forward channel, and the switching point is set at 10m / s, so that -10~0~10 (m / s) vertical take-off and landing mode, the joystick can be returned to the center; 10~50(m / s) in level flight cruise mode, the joystick can not be returned to the center; the right joystick forward channel travel in the vertical take-off and landing mode -5~0~5(m / s) ;In level flight cruise mode travel -5~0~5(m / s) or -10~0~10(deg); Right joystick side channel travel -10~0~10(m / s) or -20 ~0~20(deg); Pedal stroke -10~0~10(s -1 ) or -4~0~4 (deg).

[0071] figure 2 It is a schematic diagram of the connection between the mode switching of the aircraft and the mode conversion of the ...

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Abstract

The invention relates to the technical field of vertical take-off and landing aircraft manipulation, and provides a multi-modal fusion manipulator and a design method for an electric vertical take-off and landing tilt-rotor aircraft. The method includes: obtaining the mode switching requirements of the electric VTOL tilt-wing aircraft based on the adaptability of the multi-modal fusion manipulator and the mission characteristics of the electric VTOL tilt-wing aircraft; based on the electric VTOL tilt-wing aircraft The physical requirements of the multi-modal fusion manipulator are designed; through the physical requirements design of the multi-modal fusion manipulator, the mode conversion of the electric vertical take-off and landing tilt-wing aircraft and the information interaction of the electronic flight control system are realized. . The design method of the multi-modal fusion manipulator of the present invention realizes the manipulation of the transition stage, makes the engineering realization simpler and more convenient, and fully takes into account the task requirements and safety requirements of the transition stage.

Description

technical field [0001] The invention relates to the technical field of vertical take-off and landing aircraft manipulation, in particular to a multi-modal fusion manipulator and a design method for an electric vertical take-off and landing tilt-rotor aircraft. Background technique [0002] The electric vertical take-off and landing tilt-rotor aircraft is a new type of aircraft. It provides thrust through the electric power system, and realizes the convenience of vertical take-off and landing through the tilting of the wings. Intercity on-demand commercial operation to improve passenger and freight efficiency. [0003] HMI (Human-Machine Interface) refers to the display of manipulators and instruments. The HMI displays the aircraft status data to the pilot; the pilot obtains force feedback and status information through the HMI, and performs operations on the HMI, that is, applying instructions to the flight control system to change the aircraft status and complete the expec...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64C19/00B64C27/52B64C29/00
CPCB64C19/00B64C27/52B64C29/00Y02T50/60
Inventor 张曙光黄颖珊楚娜娜
Owner BEIHANG UNIV
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