Aircraft overshoot control method

Abstract

The invention discloses an aircraft overshoot control method comprising the following steps: S1, a flight control system is used to get the overshoot thrust, overshoot target vertical speed and overshoot target air speed of an aircraft under the current state; S2, an overshoot button is pressed, an automatic throttle pushes a throttle lever to an aircraft overshoot thrust position and is kept at a target thrust, and the aircraft looks up and increases the current vertical speed to the target vertical speed; and S3, when the vertical speed of the aircrafts rises to the target vertical speed, the aircraft increases the current air speed to the target air speed, and overshoot is completed when the current air speed rises to the target air speed. The aircraft overshoot control method is advantaged in that the overshoot target vertical speed, overshoot target air speed and overshoot target thrust of the aircraft are acquired, the aircraft completes overshoot automatically under control according to the overshoot target vertical speed, overshoot target air speed and target overshoot thrust, the problem that automatic overshoot of an aircraft cannot be controlled precisely is solved, and an effect of aircraft automatic overshoot precise control is achieved.

Description

technical field [0001] The invention relates to the technical field of flight control, in particular to an aircraft go-around control method. Background technique [0002] Automatic go-around is the process of automatically controlling the aircraft to accelerate and climb to the go-around altitude when a go-around is required. There is no automatic go-around function for manned aircraft in China, and the automatic go-around procedure for drones is similar to the automatic take-off procedure. Due to the need for automatic go-arounds, the automatic throttle can be used at low altitudes, and the thrust control method is used. However, the domestic automatic throttle has been lagging behind in development, and basically it is mechanically controlled. It only controls the speed and does not realize the control of the thrust. The thrust needs to combine the performance of the aircraft and the performance of the engine, give the thrust of the engine required to complete a certain ...

AI Technical Summary

Problems solved by technology

[0003] The object of the present invention is to provide a kind of aircraft go-around control method, to solve or at least alleviate at least one problem existing in the background technology

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