Micro-miniature unmanned plane navigation unit

A technology for a navigation device and an unmanned aerial vehicle, which is applied in the field of unmanned aerial vehicles, can solve the problems of complex calculation method of integrated navigation algorithm, long calculation period, unsuitable for the use of micro-miniature unmanned aerial vehicles (UAVs), etc.

Inactive Publication Date: 2015-04-08
北京健德乾坤导航系统科技有限责任公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] 1. The existing device has a large volume, which is not suitable for the use of micro drones, especially micro drones;
[0005] 2. The sensors used in the existing devices are relatively expensive, which is not suitable for the use of micro drones, especially micro drones;
[0006] 3. The calculation method of the existing integrated navigation algorithm is complex and the calculation period is long

Method used

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  • Micro-miniature unmanned plane navigation unit
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  • Micro-miniature unmanned plane navigation unit

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Embodiment Construction

[0032] The following describes in detail the embodiments of the present invention, examples of which are illustrated in the accompanying drawings, wherein the same or similar reference numerals refer to the same or similar elements or elements having the same or similar functions throughout. The embodiments described below with reference to the accompanying drawings are exemplary, and are intended to explain the present invention and should not be construed as limiting the present invention.

[0033] like figure 1 As shown, the micro-miniature unmanned aerial vehicle navigation device according to the embodiment of the present invention includes: a GNSS navigation module 1, an IMU navigation module 2, a geomagnetic navigation module 3, an attitude fusion and navigation control module 4 and a casing. Among them, the GNSS navigation module 1, the IMU navigation module 2, the geomagnetic navigation module 3 and the attitude fusion and navigation control module 4 are all located i...

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Abstract

The invention provides a micro-miniature unmanned plane navigation unit, comprising a GNSS (Global Navigation Satellite System) navigation module, an IMU (Inertial Measurement Unit) navigation module, a geomagnetism navigation module, a posture fusion and navigation control module and a shell; the posture fusion and navigation control module is used for receiving a plurality of data and performing data verification to judge whether the GNSS navigation module, the IMU navigation module and the geomagnetism navigation module are normal; if so, the posture fusion and navigation control module calculates a first pitching angle, a first course angle, a second pitching angle, a first roll angle, a second course angle and a second roll angle of an unmanned plane, performs posture fusion in a preset fusion algorithm, generates the position data of the unmanned plane and judges whether the position data of the unmanned plane is within the preset safety scope; and if not, the unmanned plane is controlled to adjust the in-flight status to be within the preset safety scope. With adoption of a low-cost sensor, the production cost of the whole unit can be reduced and the cross-platform navigation method is realized; and the micro-miniature unmanned plane navigation unit is applicable to the unmanned planes on different platforms.

Description

technical field [0001] The invention relates to the technical field of unmanned aerial vehicles, in particular to a navigation device for micro and small unmanned aerial vehicles. Background technique [0002] UAVs have many advantages such as low cost, low loss, zero casualties, reusability and high maneuverability, and their application scope has been expanded to the three fields of military, civilian and scientific research. In military, it can be used for reconnaissance, surveillance, attack, target simulation, early warning, etc.; in civilian use, it can be used for geodesy, meteorological observation, urban environment detection, earth resource exploration and forest fire prevention; Research, sampling and monitoring of nuclear, biological and chemical pollution areas, test verification of new technologies, new equipment and new aircraft, etc. [0003] The current UAV navigation methods include the following: landmark navigation method, dead reckoning navigation metho...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G05D1/10G05D1/08
Inventor 王根勇黄磊刘聪李学风
Owner 北京健德乾坤导航系统科技有限责任公司
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