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Aircraft operating system, aircraft method control method and aircraft

An operating system and aircraft technology, applied in the field of aircraft and aeronautical aircraft, can solve the problems of not being able to meet the comfort level of controlling the aircraft, wasting time debugging parameters, etc., and achieve the effect of protecting the experience and improving the comfort level.

Active Publication Date: 2015-10-21
杨珊珊
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] The inventor found in the process of realizing the present invention: Although the performance of the aircraft itself has been well improved in the above-mentioned technical solution, the user's operating performance has also been improved; The characteristics and operating habits are different, and the various parameters in the aircraft are set to suit the flight mode; when the user completes the flight task on a different aircraft, it is necessary to perform parameter adjustment every time, and it may also be necessary after multiple test flights. , to debug the parameters that suit you; therefore, the aircraft in the prior art cannot satisfy the user's comfort in controlling the aircraft, and it is time-consuming to debug the parameters.

Method used

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  • Aircraft operating system, aircraft method control method and aircraft
  • Aircraft operating system, aircraft method control method and aircraft
  • Aircraft operating system, aircraft method control method and aircraft

Examples

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Embodiment 1

[0038] Such as figure 1 As shown, Embodiment 1 provides an aircraft 1, including a rotor 2 that allows the aircraft 1 to rise in the air, a motor 3 that provides power to the aircraft 1, a remote control terminal 4 that issues flight commands to the aircraft, and a flight control panel that executes flight commands 5 and the ESC rack, wherein the remote control terminal 4 can be a remote control or a mobile device with remote control APP software; and also includes an aircraft operating system 6, which will be described in detail below.

[0039] Preferably, aircraft 1 is a four-axis aircraft in the present embodiment, and the mechanical structure of this aircraft can adopt double-layer propeller type multi-degree-of-freedom four-axis aircraft or a double-screw dish-shaped aircraft in the prior art; Small camera device with shooting function, cloud platform, central control unit (CPU) and information transmission device (network port).

[0040] Such as figure 2 As shown, emb...

Embodiment 2

[0065] Embodiment 2 also provides an aircraft, an operating system for the aircraft, and a control method for the aircraft. And the aircraft is provided with the same rotor 2 as in Embodiment 1, the motor 3 that provides power to the aircraft 1, the remote control terminal 4 that sends flight commands to the aircraft and the flight control panel 5 that executes the flight commands, and the electrical adjustment frame; the difference is that The operating system 6 provided by Embodiment 2 also includes a network communication unit 66 and a user account information management unit 67. After the user logs in to the user account information management unit 66, the network communication unit 67 exchanges various parameter information with the outside. Preferably, the parameter information that the user has debugged on different aircraft can be received, and these parameter information can be stored on the cloud server; specifically, the user can use the aircraft or directly through ...

Embodiment 3

[0073] Such as Figure 5 As shown, the third embodiment also provides an aircraft, an operating system for the aircraft, and a control method for the aircraft. The difference is that in this embodiment, on the basis of the first embodiment, the data exchange port is directly replaced by the network communication unit 66 and the user account information management unit 67 in the second embodiment; The beneficial effects obtained by the user account information management unit 66 and the network communication unit 67 in the second embodiment are achieved.

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Abstract

The invention provides an aircraft operating system, an aircraft method control method and an aircraft. The operating system comprises a first memory cell used for storing aircraft factory configuration parameters; a second memory cell used for storing individual parameters set by users on an aircraft; a data exchange port used for exchanging data relevant to aircraft configuration with an external storage medium; a selection unit used for selecting parameters from the first memory cell and / or the second memory cell and / or the data exchange port; and a control unit used for updating parameters in the aircraft in dependence on the parameter information selected by the selection unit. Accordingly, in controlling different aircraft devices, only by inserting a portable storage medium into the data exchange port can a user rapidly select a suitable operation mode by debugging.

Description

technical field [0001] The invention relates to the technical field of aviation aircraft, in particular to an aircraft operating system, an aircraft control method and the aircraft. Background technique [0002] With the advancement of electronic science and technology and the development of the computer industry, various types of aircraft have gradually entered the field of people's lives. For example, in some occasions such as filming, item delivery, and flight performances, aircraft are often required to perform corresponding tasks; It is precisely because of this demand that the technology of aircraft has been well developed. [0003] For example, in the Chinese patent application number CN201410187335.9, a double-layer propeller multi-degree-of-freedom four-axis aircraft is disclosed. The double-layer propeller structure is located on the top of the power cabin, and the vertical rotation control mechanism is arranged on the power cabin. The side of the cam is connected...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G05D1/10
Inventor 杨珊珊
Owner 杨珊珊
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