Unmanned aerial vehicle three-dimensional trajectory guidance method based on inverse dynamics

An inverse dynamics, three-dimensional trajectory technology, applied in three-dimensional position/channel control, non-electric variable control, control/regulation system and other directions, can solve the problems of control effect coupling effect and other problems, achieve convenient parameter setting, clear physical meaning, Simple control structure

Active Publication Date: 2017-05-31
BEIHANG UNIV
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Problems solved by technology

[0010] It can be seen from formula (1) (2) that (V g , χ, γ) and (T, α, β, μ) are mutually coupled control variables, if the traditional PID control is adopted, the control effect will be seriously affected by the coupling effect

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  • Unmanned aerial vehicle three-dimensional trajectory guidance method based on inverse dynamics
  • Unmanned aerial vehicle three-dimensional trajectory guidance method based on inverse dynamics
  • Unmanned aerial vehicle three-dimensional trajectory guidance method based on inverse dynamics

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Embodiment Construction

[0058] The present invention will be further described in detail with reference to the accompanying drawings and embodiments.

[0059] The present invention is an unmanned aerial vehicle three-dimensional trajectory guidance method based on inverse dynamics. By combining the analytical method and the numerical iteration method, the position state equation of the unmanned aerial vehicle is sequentially solved by first-level inverse dynamics, and the unmanned aerial vehicle is The ground speed and track angle state equations are solved by two-level inverse dynamics, and the command thrust, command angle of attack and command track roll angle of the UAV are obtained, and then these commands are input into the designed attitude control The loop can control the actual ground speed and position of the UAV. At the same time, PID control is used to make the actual position of the UAV converge on the reference trajectory between waypoints.

[0060] The structure block diagram of the wh...

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Abstract

The invention discloses an unmanned aerial vehicle three-dimensional trajectory guidance method based on inverse dynamics and belongs to the technical field of unmanned air vehicle navigation guidance and control. The method comprises the following steps: firstly, performing primary inverse dynamics resolving on position state equations of the unmanned aerial vehicle by combining an analytical method and a numerical iteration method at the aim of a certain trajectory section of a certain unmanned aerial vehicle, and performing secondary inverse dynamics resolving on ground velocity and track angle state equations of the unmanned aerial vehicle so as to obtain the command thrust, command attack angle and command track roll angle of the unmanned aerial vehicle; inputting the command quantities into the designed attitude control loop so as to control the actual ground velocity and position of the unmanned aerial vehicle, and enabling the actual position of the unmanned aerial vehicle to be convergent to a reference trajectory between way points by adopting PID (Proportion Integration Differentiation) control. According to the method disclosed by the invention, the ground velocity and three-dimensional position of the unmanned aerial vehicle can be simultaneously and accurately controlled, the expected flight path of the unmanned aerial vehicle is adjusted on line, and the controller computing cost is low.

Description

technical field [0001] The invention belongs to the technical field of navigation, guidance and control of unmanned aerial vehicles, and in particular relates to a three-dimensional trajectory guidance method for unmanned aerial vehicles based on inverse dynamics. Background technique [0002] UAVs, also known as unmanned aerial vehicles, are widely used in military and civilian fields; UAV guidance refers to making UAVs fly along a given trajectory through command programs. With the increasingly diverse tasks performed by UAVs, people's requirements for the maneuverability of UAVs are also increasing. The traditional two-dimensional trajectory guidance law can no longer meet the demand. Realizing high-precision tracking control of three-dimensional trajectories can make UAVs It is of great significance to complete special tasks such as terrain avoidance, formation flight and autonomous aerial refueling. [0003] In the trajectory tracking control of UAVs, it is of great pr...

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G05D1/10
CPCG05D1/101
Inventor 王宏伦吴健发李娜姚鹏苏子康
Owner BEIHANG UNIV
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