Speed vector directive driving method for unmanned aerial vehicle human-in-the-loop head-up display

A technology of velocity vector and driving method, which is applied in the field of aircraft avionics, and can solve problems such as the difficulty in obtaining the real angle of attack of drones

Active Publication Date: 2020-04-24
JIANGXI HONGDU AVIATION IND GRP
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] However, for UAVs, considering the cost of use or measurement accuracy, the angle of attack sensor is generally not installed, and it is difficult to obtain the rea

Method used

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  • Speed vector directive driving method for unmanned aerial vehicle human-in-the-loop head-up display
  • Speed vector directive driving method for unmanned aerial vehicle human-in-the-loop head-up display
  • Speed vector directive driving method for unmanned aerial vehicle human-in-the-loop head-up display

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Embodiment Construction

[0022] The technical solutions in the embodiments of the present invention are clearly and completely described below.

[0023] According to the calculation method described in the present invention, calculate false angle of attack, in order to illustrate the validity of false angle of attack, in the simulation of aircraft six degrees of freedom, the normal angle of attack of the false angle of attack of construction and aircraft equation output is compared, figure 1 It is the simulation comparison when the simulation time is 2s ~ 6s when the half rod is pulled longitudinally, figure 2 For the simulation comparison when the rod is fully stretched longitudinally, image 3 It is a simulation comparison of pushing the full pole vertically.

[0024] From the simulation results, it can be seen that the response polarity of the false angle of attack is correct during maneuvering, and there is basically no delay. In the manipulation of small and medium sticks, the response amplitud...

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Abstract

The invention provides a speed vector directive driving method for unmanned aerial vehicle human-in-the-loop head-up display. According to the method, under the condition that no effective attack angle signal is measured, according to the correlation derivation of angle-of-attack change and normal overload increment, a pseudo angle of attack is constructed on a ground console by using effective normal overload information downloaded by an unmanned aerial vehicle to simulate a real angle of attack, so that the pseudo angle of attack is used for driving the display of a head-up display speed vector directive of a flight control comprehensive picture display area of the ground console. According to the method, the response polarity of the pseudo angle of attack is correct and basically free of delay in the maneuvering process of the unmanned aerial vehicle, the response amplitude basically coincides with that of a normal angle of attack in the operation of medium and small rods, and the response amplitude is slightly smaller than that of a normal angle of attack in the operation of a large rod, so that the use requirements are met.

Description

technical field [0001] The invention belongs to the field of aircraft avionics, in particular to a method for driving a speed vector indicator for a UAV HUD display. Background technique [0002] In the design of UAV operation and control, refer to the display effect of the head-up display in the cockpit of the manned aircraft, refer to the human-in-the-loop control similar to the manned mode, and add or replace the specific flight parameters of the UAV in detail processing, real-time display The current flight environment of the UAV provides the operator with important information required for flight control and provides an important guarantee for the safe flight of the aircraft. [0003] In the display area of ​​the UAV flight control comprehensive screen, the use of the speed vector symbol is very important. By observing the relative positional relationship between the symbol and the horizon, the UAV operator can easily grasp the change of the current flight altitude of t...

Claims

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Application Information

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IPC IPC(8): G01P1/07G01D7/06
CPCG01D7/06G01P1/07
Inventor 张羽白李玉飞肖成方郭枚林冷国旗邹俊俊涂慧玲刘宝文范钦海相梅翁雪花陈孔锦
Owner JIANGXI HONGDU AVIATION IND GRP
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