Fixed-wing unmanned aerial vehicle obstacle avoidance robust anti-interference flight control method based on preset performance

A flight control and preset performance technology, applied in the field of aircraft control, can solve the problems of closed-loop unmanned aerial vehicle system instability, unmanned aerial vehicles difficult to achieve flight performance, etc., to achieve the effect of ensuring safe flight

Active Publication Date: 2021-07-23
NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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AI Technical Summary

Problems solved by technology

However, studying the transient performance plays an important role in improving the performance of the UAV flight control system; for example, excessive overshoot may cause the UAV actuator to exceed the physical limit, resulting in the instability of the closed-loop UAV sy

Method used

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  • Fixed-wing unmanned aerial vehicle obstacle avoidance robust anti-interference flight control method based on preset performance
  • Fixed-wing unmanned aerial vehicle obstacle avoidance robust anti-interference flight control method based on preset performance
  • Fixed-wing unmanned aerial vehicle obstacle avoidance robust anti-interference flight control method based on preset performance

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Embodiment Construction

[0106] The technical solution of the present invention will be further described below in conjunction with the accompanying drawings.

[0107] Such as figure 1 As shown, the fixed-wing UAV obstacle avoidance and anti-disturbance flight control method based on preset performance of the present invention includes the following steps:

[0108] (1) Generate an initial route, adjust the slope, curvature and safety altitude of the initial route to generate a continuous safe flight route for the UAV;

[0109] (2) Neglecting the interaction between lateral motion and longitudinal motion, establish a UAV longitudinal model with external interference and define a performance function;

[0110] (3) Based on the longitudinal model of the UAV, respectively design the height controller, speed and track inclination angle controller based on the preset performance function;

[0111] (4) Design a disturbance observer, and design an attitude angle controller and an attitude angle rate control...

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Abstract

The invention discloses a fixed-wing unmanned aerial vehicle obstacle avoidance anti-interference flight control method based on preset performance, and the method comprises the following steps: generating an initial route, adjusting the parameters of the initial route, and generating a continuous safe flight route of an unmanned aerial vehicle; neglecting the mutual influence of transverse and lateral movement and longitudinal movement, establishing an unmanned aerial vehicle longitudinal model with external interference, and defining a performance function; based on the longitudinal model of the unmanned aerial vehicle, designing a height controller and a speed and track inclination angle controller based on a preset performance function; designing a disturbance observer, and designing an attitude angle controller and an attitude angle rate controller based on the disturbance observer; selecting a Lyapunov function of a control system, selecting control parameters according to the Lyapunov stability theory, and ensuring that system signals are bounded. According to the method, safe flight of the fixed-wing unmanned aerial vehicle can be ensured, the height tracking error can meet the given performance, and robust anti-interference tracking flight control of the fixed-wing unmanned aerial vehicle under external interference is realized.

Description

technical field [0001] The invention relates to aircraft control technology, in particular to an obstacle avoidance and anti-disturbance flight control method for a fixed-wing unmanned aerial vehicle based on preset performance. Background technique [0002] During the First World War, the United States introduced military drones, which promoted the application of drones in the military field. So far, it has developed the Global Hawk, Pterosaur, Predator, Sword, X47-B And a variety of advanced military drones such as fire scouts. At the same time, drones are also widely used in civilian fields such as aerial photography and agriculture. The flight control system is the main component of the UAV system, and it is the basis for performing various flight tasks and flying safely. An important research direction of technology. [0003] In the existing tracking control methods of fixed-wing UAV systems, they usually focus on how to ensure that the tracking error converges to a b...

Claims

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Application Information

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IPC IPC(8): G05D1/08G05D1/10
CPCG05D1/0808G05D1/101
Inventor 邵书义陈谋姜斌张柯盛守照甄子洋
Owner NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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