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Robust and anti-disturbance flight control method for fixed-wing unmanned aerial vehicles 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: 2022-06-28
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 system
Therefore, when designing a robust and anti-disturbance flight controller for safe obstacle avoidance, only considering the steady-state performance without considering the transient performance will make it difficult for the UAV to achieve the desired flight performance

Method used

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  • Robust and anti-disturbance flight control method for fixed-wing unmanned aerial vehicles based on preset performance
  • Robust and anti-disturbance flight control method for fixed-wing unmanned aerial vehicles based on preset performance
  • Robust and anti-disturbance flight control method for fixed-wing unmanned aerial vehicles 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] like 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 controller...

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Abstract

The invention discloses an obstacle-avoiding and anti-disturbance flight control method for a fixed-wing unmanned aerial vehicle based on preset performance. Interaction between lateral motion and longitudinal motion, establish a UAV longitudinal model with external interference and define performance functions; based on UAV longitudinal model, design altitude controller, speed and track inclination angle based on preset performance functions Controller; design a disturbance observer, design an attitude angle controller and an attitude angle rate controller based on the disturbance observer; select the Lyapunov function of the control system, select the control parameters according to the Lyapunov stability theory, and ensure the boundedness of the system signal . The invention can ensure the safe flight of the fixed-wing unmanned aerial vehicle, and can also make the height tracking error meet the given performance, and realize the robust anti-disturbance tracking flight control of the fixed-wing unmanned aerial vehicle under external interference.

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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Patent Type & Authority Patents(China)
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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