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Control method and control terminal of aircraft

A control terminal and control method technology, applied in attitude control, non-electric variable control, control/adjustment system, etc., can solve problems such as hidden safety hazards, aircraft friction, aircraft formation confusion, etc., to improve practicability and ensure safety. Effect

Active Publication Date: 2016-08-24
TENCENT TECH (SHENZHEN) CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] However, when multiple people control multiple aircraft at the same time, it is difficult to maintain the consistency of the aircraft during the flight, and it is easy to cause confusion in the formation of the aircraft, or due to improper operation, the aircraft will rub and collide with each other, resulting in a greater safety hazard

Method used

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  • Control method and control terminal of aircraft

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Embodiment Construction

[0036] The embodiment of the present invention provides an aircraft control method and a control terminal, which can simultaneously control multiple aircrafts to fly without colliding with each other by one control terminal, ensuring the safety during the flight, and enabling the aircraft to They work collaboratively and maintain formation during flight, which is beneficial for the operator to control it and improve the practicability of the scheme.

[0037] The terms "first", "second", "third", "fourth", etc. (if any) in the description and claims of the present invention and the above drawings are used to distinguish similar objects, and 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 that the embodiments of the invention described herein are, for example, capable of practice in sequences other than those illustrated or described herein. Furthermore, the t...

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Abstract

The embodiment of the invention discloses a control method of an aircraft. The method is applied to at least one aircraft cooperative group which comprises a control terminal, a master unit and at least one slave unit. The method comprises the following steps: when the aircraft is in a flying state, receiving current flying information transmitted by the master unit and the slave units; determining a flying error value of each slave unit according to the current flying information of the master unit and the slave units; generating a first control instruction of the master unit according to the current flying information of the master unit, and generating a second control instruction of the slave units according to the current flying information and the flying error value of the slave units; transmitting the first control instruction to the master unit, and transmitting the second control instruction to the slave units. The embodiment of the invention further provides the control terminal. One control terminal can be used for simultaneously controlling a plurality of aircrafts to fly under a condition of no mutual collision, to guarantee the safety during flying and keep a formation during flying; the control terminal is favorable for letting an operator control the aircraft.

Description

technical field [0001] The invention relates to the technical field of unmanned aircraft, in particular to an aircraft control method and a control terminal. Background technique [0002] The unmanned aircraft is referred to as "aircraft" for short, and the aircraft is an unmanned aircraft that utilizes radio remote control telemetry equipment and its own program control device. Multiple aircrafts can be arranged in various queues during the flight for reconnaissance or performance. [0003] Usually, at the same time, the user can only control one aircraft through one control terminal. If multiple aircrafts are to be controlled simultaneously, multiple users are required to use different control terminals to simultaneously control multiple aircrafts. [0004] However, when multiple people control multiple aircraft at the same time, it is difficult to maintain the consistency of the aircraft during the flight, and it is easy to cause confusion in the formation of the aircra...

Claims

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Application Information

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IPC IPC(8): G05D1/08G05D1/10
CPCG05D1/0816G05D1/101
Inventor 申俊峰王洁梅杨瑞波荆彦青
Owner TENCENT TECH (SHENZHEN) CO LTD
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