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Flight evaluation system and method based on small multi-rotor aircraft

A technology of multi-rotor aircraft and evaluation system, applied in the field of flight evaluation system based on small multi-rotor aircraft

Active Publication Date: 2021-07-23
BEIJING FORESTRY UNIVERSITY
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

If the performance requirements, index system, evaluation methods and evaluation criteria of miniaturized multi-rotor aircraft are copied from the standards and scales of manned aircraft, there are obviously certain limitations and inadaptability. The flying effect is very different

Method used

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  • Flight evaluation system and method based on small multi-rotor aircraft
  • Flight evaluation system and method based on small multi-rotor aircraft
  • Flight evaluation system and method based on small multi-rotor aircraft

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Embodiment Construction

[0051] Next, the technical solutions in the embodiments of the present invention will be described in contemplation in the embodiment of the present invention, and it is clear that the described embodiments are intended to be in an embodiment of the invention, not all of the embodiments of the invention. Based on the embodiments of the present invention, there are all other embodiments obtained without making creative labor without making creative labor premises.

[0052] It should be understood that when used in this specification and the appended claims, the terms "include" and "including" indicating the description of the features, overall, steps, operations, elements, and / or components, but does not exclude one or Multiple other features, overall, steps, operations, elements, components, and / or their set presence or addition.

[0053] In the present embodiment, the small multifocal aircraft illustrates four-rotor aircraft; wherein the aircraft they own have a controller, e...

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Abstract

The embodiment of the invention discloses a flight evaluation system and method based on a small multi-rotor aircraft. The system comprises an import module which is used for importing initial data and carrying out system initialization, a ground station module which is used for displaying flight environment data and path planning of the aircraft, a data module which is used for feeding back the detected flight data in real time, meanwhile, carrying out data budgeting, a control module which is used for automatically controlling and adjusting the aircraft according to the deviation generated by the data budgeting and the real-time flight environment data, a state module which is used for monitoring, simulating and recording the state of the aircraft when the aircraft is in a stable state, and a quality evaluation module which is used for outputting and comparing the data obtained through monitoring simulation with a preset evaluation index to obtain an evaluation result and displaying the evaluation result. According to the flight evaluation system and method based on the small multi-rotor aircraft of the invention, a set of evaluation system is constructed according to the characteristics of the small-sized multi-rotor aircraft, so that a reference effect is also achieved for the design, development and test of the unmanned aerial vehicle.

Description

Technical field [0001] The present invention relates to the field of aircraft assessment, and more particularly to a flight assessment system and method based on a small multifocal aircraft. Background technique [0002] The flight quality is the most concerned issue of the aircraft designer and manipulator, and always play an important role in the design, development, testing and use of the aircraft. Good flying quality is an important guarantee for ensuring the safe flight of the aircraft and successfully completing the established flight task. [0003] A multi-rotor drone refers to an unmanned flight device that can be manipulated by a remote control, or a machine itself is able to perform unmanned flight of unmanned flights. Its rot w can generally have even several structures such as 4 axes, 8 axes, mainly including two models of "X" and "+" type. The rotor is uniformly distributed around the body, and the pitch and bullow are paired. By controlling the rotational speed of t...

Claims

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Application Information

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IPC IPC(8): G05D1/10
CPCG05D1/101Y02T90/00
Inventor 胡春鹤张军国李恒宝柴垒
Owner BEIJING FORESTRY UNIVERSITY