Navigation device and aircraft

A technology of navigation equipment and aircraft, applied in the direction of instruments, three-dimensional position/course control, non-electric variable control, etc., can solve the problems of poor stability and anti-interference, and achieve the effect of making up for the single guidance method

Pending Publication Date: 2020-11-20
BEIJING INFORMATION SCI & TECH UNIV
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] The embodiment of the present application provides a navigation device and an aircraft to at least solve the problem that the current aircraft relies on an inertial navigation module composed of a gyroscope and an acceleration sensor to navigate the aircraft. When facing a high dynamic environment, its stability and anti-interference are relatively low. poor technical problem

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  • Navigation device and aircraft
  • Navigation device and aircraft
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Embodiment Construction

[0024] In order to enable those skilled in the art to better understand the solution of the present application, the technical solution in the embodiment of the application will be clearly and completely described below in conjunction with the accompanying drawings in the embodiment of the application. Obviously, the described embodiment is only It is an embodiment of a part of the application, but not all of the embodiments. Based on the embodiments in this application, all other embodiments obtained by persons of ordinary skill in the art without creative efforts shall fall within the scope of protection of this application.

[0025] It should be noted that the terms "first" and "second" in the description and claims of the present application and the above drawings are used to distinguish similar objects, but not necessarily used to describe a specific sequence or sequence. It is to be understood that the data so used are interchangeable under appropriate circumstances such...

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Abstract

The invention discloses a navigation device and an aircraft. The navigation device comprises a sensor, a controller, a power supply module and an ignition device, and the sensor is used for collectingmotion data of an aircraft. The controller is connected with the sensor and used for generating a navigation instruction according to the motion data and controlling the ignition device to correct the flight attitude of the aircraft according to the navigation instruction. The ignition device is connected with the controller and used for correcting the flight attitude of the aircraft. The power supply module is used for supplying power to the sensor, the controller and the ignition device. According to the application, the technical problem that the stability and the anti-interference performance of the existing aircraft are poor when the aircraft is navigated by virtue of an inertial navigation module consisting of a gyroscope and an acceleration sensor in a high-dynamic environment is solved.

Description

technical field [0001] The present application relates to the field of navigation equipment, in particular, to a navigation equipment and an aircraft. Background technique [0002] Aircraft is a product of the industrial revolution in the 19th century. With the birth of various aircraft, the use scenarios of aircraft in various civilian and military applications continue to expand. In the 1990s, aircraft began to develop rapidly and be widely used, and various types of aircraft emerged in an endless stream. In recent years, aircrafts have gradually developed towards the direction of miniaturization, lightness, and intelligence, which put forward higher requirements for the navigation control of aircrafts. Aircrafts need to achieve stronger autonomous navigation flight capabilities in as small a space as possible. Complete specific flight missions in dangerous environments. In order to maintain the stable flight of the aircraft, the traditional aircraft is equipped with a g...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G05D1/08G05D1/10
CPCG05D1/0808G05D1/101
Inventor 刘宁苏中袁超杰李擎戚文昊刘福朝付国栋
Owner BEIJING INFORMATION SCI & TECH UNIV
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