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Wireless flight remote controller for unmanned airship and wireless flight remote control method of remote controller

A technology of flight remote control and unmanned airship, applied in the field of remote control engineering of unmanned airship, to avoid wear and tear and to use flexibly

Inactive Publication Date: 2013-03-20
CHINESE AERONAUTICAL RADIO ELECTRONICS RES INST
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0007] The present invention aims to solve the problems existing in the existing airship remote controllers, and provides a wireless flight remote controller suitable for unmanned airships and its wireless flight remote control method
The wireless flight remote controller transmits the collected control signal to the ground station through wireless RS485, and then the ground station transmits it to the unmanned airship through a unified link, which not only solves the problem of switching the wireless communication link when using the ordinary aircraft model remote controller. The problem also frees the flight controller outside the cabin from the shackles of the wired remote control, ensuring the flight safety of the airship

Method used

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  • Wireless flight remote controller for unmanned airship and wireless flight remote control method of remote controller
  • Wireless flight remote controller for unmanned airship and wireless flight remote control method of remote controller
  • Wireless flight remote controller for unmanned airship and wireless flight remote control method of remote controller

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Embodiment Construction

[0029] The present invention will be further described below in conjunction with specific implementation examples.

[0030] A wireless flight remote control suitable for drones, such as figure 1 As shown, potentiometer knob and rocker mechanism 1, analog signal acquisition module 2, wireless RS485 communication module 3 and antenna 4, battery 5, power processing module 6 and battery voltmeter 7.

[0031] Such as figure 2 As shown, the potentiometer knob and rocker mechanism 1 includes a ducted steering knob 8 , an engine mixing ratio knob 9 , a two-degree-of-freedom rocker 10 and a single-degree-of-freedom rocker 11 . The duct steering knob 8 controls the duct direction of the unmanned airship, and the starting position is 0 degrees in the middle, which can be turned clockwise or counterclockwise; the engine mixing ratio knob 9 controls the mixing ratio control amount of the engine, and the starting position is 0 degrees on the left side. degree, the mixing ratio control am...

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Abstract

The invention discloses a wireless flight remote controller for an unmanned airship, which comprises a remote controller housing, a knob potentiometer, a rocker mechanism, an analog signal acquisition module, a wireless RS485 (recommended standard 485) transport module and an antenna, a battery and a power supply processing module, wherein the wireless flight remote controller transmits an acquired control signal to a ground station in a wireless RS485 mode, and then the ground station transmits the control signal to the unmanned airship by a unified link. The remote controller can allow the unmanned airship to keep a communication link in each flight stage, without switching; a manipulator outside a compartment is flexible to use; and an activity range is not restrained.

Description

technical field [0001] The invention relates to the technical field of remote control engineering for unmanned airships, in particular to a wireless flight remote controller for unmanned airships and an implementation method thereof. Background technique [0002] Unmanned airship is a kind of aircraft that relies on air buoyancy and can be controlled. It can carry different types of surveillance equipment for low-cost and long-duration flight, so it has a wide range of military and commercial applications. The flight process of an airship is divided into three parts: takeoff, cruise, and landing. During the cruising phase, the surrounding environment of the airship is relatively stable, and there is no need to make large-scale adjustments to the flight speed and attitude of the airship, so the flight control system in the cabin of the ground station can usually meet the requirements. However, during the take-off and landing stages of the airship, the speed of the unmanned a...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G05D1/10G08C17/02
Inventor 方力
Owner CHINESE AERONAUTICAL RADIO ELECTRONICS RES INST
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