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Composite recognition method for flight dynamics model of unmanned helicopter

An unmanned helicopter and flight dynamics technology, applied in the field of aerospace and unmanned aerial vehicles, can solve the problems of helicopter excitation, failure to solve the problem of helicopter flying out of sight, limited experiment time, etc., and achieve the effect of ensuring flight safety

Inactive Publication Date: 2011-05-25
TSINGHUA UNIV
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AI Technical Summary

Problems solved by technology

However, constant acceleration, accurate acceleration distance and flight speed maintenance after the start of the experiment are all observed and manipulated by ground operators, and its accuracy is difficult to guarantee
In addition, since the constant acceleration method cannot solve the problem of the helicopter flying out of sight, the time of the experiment is very limited, so it is difficult to sufficiently stimulate the helicopter

Method used

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  • Composite recognition method for flight dynamics model of unmanned helicopter
  • Composite recognition method for flight dynamics model of unmanned helicopter
  • Composite recognition method for flight dynamics model of unmanned helicopter

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Embodiment Construction

[0018] The composite identification method of unmanned helicopter flight dynamics model is mainly composed of unmanned helicopter (1), flight control computer (2), data station (3), ground station (4), remote control transmitter (5) and remote control receiver (6 ) and other components.

[0019] The ground station (4) is used for monitoring the flight of the unmanned helicopter (1) through the data station (3). The flight control computer (2) is used for auxiliary manipulation of the unmanned helicopter (1), on the one hand to ensure the flight safety of the unmanned helicopter (1), and on the other hand to ensure that its flight state does not change too much. Since the control algorithms such as PID can obtain the controller parameters without the need of a dynamic model, the controller parameters can be obtained through debugging in actual flight, so the flight control computer (2) can first use this type of control algorithm. After the identification experiment, the fligh...

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Abstract

The invention discloses a composite recognition method for a flight dynamics model of an unmanned helicopter, which belongs to the field of unmanned aerial vehicle dynamics modeling. The composite recognition method is characterized in that: the unmanned helicopter, a flight control computer, a data station, a ground station, a remote control transmitter and a remote control receiver are involved, wherein the flight control computer is used for assisted control for a recognition experiment to keep the relatively more stable flight conditions such as speed and height of the helicopter at the same time of ensuring the flight safety of the helicopter; a ground operator triggers the dynamic response of the helicopter by a remote control instruction; and the flight control computer adds the remote control instruction into the control input of the unmanned helicopter and records the remote control instruction together with an automatic control instruction for dynamic recognition after a flight experiment. In the method, manual remote control and assisted automatic control are simultaneously introduced, so that the flight dynamics model of the unmanned helicopter can be precisely and safely recognized.

Description

technical field [0001] The invention is a method for identifying the flight dynamics model of an unmanned helicopter, which can safely, accurately and fully identify the flight dynamics model of the unmanned helicopter. It is mainly used in technical fields such as aerospace and drones. Background technique [0002] The flight dynamics model of an unmanned helicopter reflects the control response characteristics of the helicopter to the control input in the flight state. The traditional method is that during the flight of the helicopter, the pilot applies manipulation instructions to the helicopter to stimulate the helicopter to make a dynamic response. This method has been successfully demonstrated on a manned helicopter. [0003] However, this method is difficult to apply on unmanned helicopters. The main reason is that, unlike manned helicopters, the operators of unmanned helicopters need to observe and operate the helicopter with the naked eye on the ground. Therefor...

Claims

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Application Information

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IPC IPC(8): G05B17/02
Inventor 王冠林朱纪洪
Owner TSINGHUA UNIV
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