Aircraft emergency control device and control method thereof

A technology of emergency control and control method, applied in the direction of non-electric variable control, control/adjustment system, three-dimensional position/course control, etc., can solve the problem of not being able to effectively protect the safe flight of aircraft, the high proportion of flight accidents, and affecting the safety of aircraft Use and other issues to achieve the effect of avoiding accidental crashes, light weight, and simple structure

Inactive Publication Date: 2016-08-03
至简天蕴智控科技(苏州)有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] The remote control signals of existing multi-rotor aircraft are basically based on radio signals in the frequency band 2.4G, and the remote control equipment has frequency hopping settings to minimize the mutual interference of remote control signals in the same band, but in general, the remote control signals are vulnerable to various obstacles The communication distance is limited, and even with the frequency hopping setting, it is not enough to completely resist the interference of all other remote control signals of the same band
[0004] When the remote control signal of the aircraft is interfered, the aircraft will often lose control and fly away from the set route or area autonomously, eventually leading to flight accidents. According to incomplete statistics, the proportion of such flight accidents is higher than that caused by aircraft hardware failures. The proportion of flight accidents is much higher, which greatly affects the safe use of aircraft
[0005] Most of the existing commercial aircraft, when the remote control signal interferes, first try to repeat the connection manually or automatically. After the repeated connection is successful, you can continue to control the aircraft. Through this button, the aircraft is controlled to fly to a fixed position, so as to avoid the occurrence of flight accidents. Although the above-mentioned technical process looks foolproof on the surface, a large number of flight accident examples after the remote control signal is lost tell us that this design is not 100% % of them work, and the failure rate is quite high. Countless complaints of this kind can be seen from the forum of a famous aircraft company, indicating that the above-mentioned technical process has not fundamentally solved the problem
[0006] In the prior art, it involves the use of GSM communication technology and GPS positioning technology for aircraft self-rescue and recovery. These patents have added GSM transmitters, GPS receiver modules, GPS decoders and other equipment. When the aircraft loses contact, through The GSM transmitter transmits the GPS positioning signal to the user to facilitate the search for the missing aircraft, but in fact, the existing commercial aircraft already has similar functions, and it does not need an independent GSM transmitter module to transmit the GPS signal when the aircraft was last missing. , and even the video signal of the camera equipped on the aircraft is saved and uploaded by various means, and finally provided to the user, so that the user can retrieve the missing aircraft, and many users have already found their lost aircraft through this method. Although this type of technology can provide users with an auxiliary means to retrieve the missing aircraft, it cannot change the reality that the aircraft has disappeared and crashed. What users often find is a damaged aircraft, or even completely unusable. Therefore, This type of technology cannot effectively protect the safe flight of the aircraft

Method used

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  • Aircraft emergency control device and control method thereof
  • Aircraft emergency control device and control method thereof

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0049] Set the aircraft emergency control equipment to accept ordinary GSM communication signals, and insert the SIM card that has activated the communication service, you can communicate with the SIM card by dialing the specific number of the SIM card or by SMS.

[0050] When the aircraft loses the remote control signal and cannot use the "one-key return" function, the user can quickly re-establish contact with the aircraft in the following ways:

[0051] Dial the specific number of the SIM card or send any text message to the SIM card. After a few seconds, the communication signal receiving and feedback module on the aircraft receives the incoming call signal or text message, and immediately feeds back the signal to the flight control system processor of the aircraft. Make the aircraft enter the preset emergency flight mode, as follows:

[0052] A terminates the scheduled flight, enters the hover mode, and waits for the user to reconnect the remote control signal to regain c...

Embodiment 2

[0061] When the aircraft is in a flight area where signals cannot be transmitted through ground base stations, such as oceans, deserts, virgin forests, etc., a module that can receive maritime satellite signals can be used, and a SIM card that has activated communication services can be inserted. You can dial the SIM card Specific number or communicate with this SIM card by short message etc., control process can be the same as embodiment 1.

Embodiment 3

[0063] Further, a corresponding button recognition program can be developed in the flight control system processor, and a specific button is defined as a specific flight mode in the emergency flight control system; with the communication signal receiving and feedback module, when dialing the specific number of the SIM card After that, the phone is automatically connected, and the user can control the emergency state of the aircraft through the number buttons on the communication terminal operated by the user.

[0064] The specific control process is as follows:

[0065] Assume that the number buttons 1, 2, and 3 are enabled, and the flight modes defined by them are as follows:

[0066] Button No. 1: Terminate the scheduled flight, enter the hovering mode, wait for the user to reconnect the remote control signal, and regain control;

[0067] Button No. 2: land directly on the spot;

[0068] Button 3: Enter the one-button return mode, fly to the preset position and land, such ...

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PUM

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Abstract

The invention discloses an aircraft emergency control device and a control method. The aircraft emergency control device includes a communication signal receiving and feedback module (1) and an aircraft control system processor (2); the communication signal receiving and feedback module (1) receives instruction signals sent by a ground base station or instruction signals sent by a satellite, and transmits the received signals to the aircraft control system processor (2); the aircraft control processor system comprises a microprocessor module (3) and an emergency control module (4); and the output end of the microprocessor module (3) is connected with the input end of the emergency control module (4), so that an aircraft can enter a preset emergency flight mode. According to the aircraft emergency control device and the control method of the invention, the communication signal receiving and feedback module is just additionally adopted, and the combinations of various kinds of communication signals or key combinations which are simple in logic are adopted in cooperation, and therefore, flight control can be performed on the aircraft losing remote control signals, and the crash of the aircraft due to being out of control can be avoided.

Description

technical field [0001] The invention belongs to the field of aircraft equipment, and in particular relates to an aircraft emergency control equipment and a control method thereof. Background technique [0002] The structure of multi-rotor aircraft is relatively simple, the cost is low, the performance is excellent, the flight control technology is relatively complete, and it has broad application prospects. It has become a popular hot spot in the world. [0003] The remote control signals of existing multi-rotor aircraft are basically based on radio signals in the frequency band 2.4G, and the remote control equipment has frequency hopping settings to minimize the mutual interference of remote control signals in the same band, but in general, the remote control signals are vulnerable to various obstacles The communication distance is limited, and even with the frequency hopping setting, it is not enough to completely resist the interference of all other remote control signals...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G05D1/10
CPCG05D1/101
Inventor 杨小韬
Owner 至简天蕴智控科技(苏州)有限公司
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