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Small-sized depopulated helicopter independent flight control system

A flight control system, unmanned helicopter technology, applied in control/adjustment system, attitude control, comprehensive factory control, etc. limited issues

Active Publication Date: 2009-06-03
SHENYANG INST OF AUTOMATION - CHINESE ACAD OF SCI
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] However, in the prior art, unmanned helicopters have achieved pre-programmed stable flight, but compared with manned aircraft and remote-controlled model aircraft, their maneuverability is very limited, and they do not yet have the ability to complete tasks autonomously, especially is a military mission capability
Therefore, the autonomous capability and system reliability of unmanned helicopters cannot meet the requirements at present, and the application range of unmanned helicopters is limited, making it impossible to complete a given task within the beyond visual range

Method used

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  • Small-sized depopulated helicopter independent flight control system
  • Small-sized depopulated helicopter independent flight control system
  • Small-sized depopulated helicopter independent flight control system

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Embodiment Construction

[0020] Below in conjunction with accompanying drawing and embodiment describe the present invention in detail:

[0021] see figure 1 , the autonomous flight system of unmanned helicopters, including two parts: the airborne control system and the ground control system, of which:

[0022]The airborne control system 2 consists of an airborne computer 8 (using a PC-104 industrial computer), an airborne sensor group, a digital signal processor (DSP), an airborne wireless Ethernet access point (Access Point) AP1, and a remote control signal receiving The airborne computer obtains the signals of each sensor through the RS-232 serial communication interface, and connects with the ground wireless Ethernet access point AP2 through the airborne wireless Ethernet access point AP1 (the airborne computer As the core of the airborne part, it plays the role of data collection, data processing, and data storage. Through the 802.11g network protocol, the wireless AP and the ground control syst...

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Abstract

The invention relates to a miniature unmanned helicopter auto flight control system which comprises an on-board control system, wherein, an on-board computer gets signals from sensors through a serial port, and exchanges data with a ground-based computer through on-board and ground wireless Ethernet access points; the on-board computer carries out serial communication with a digital signal processor to control a steering engine set of the unmanned helicopter; a remote control signal receiver outputs to the digital signal processor and then is connected with the on-board computer through a serial port, and an auto control signal and a ground remote control signal are accumulated to get a current steering engine control signal. And the auto flight control system also comprises a ground control system, wherein, the ground-based computer transmits flight control instructions to the on-board computer and receives and records flight data; through operating a ground helicopter remote controller, manual control instructions can be transmitted to the on-board remote control signal receiver via wireless radio frequency signals. The invention can improve the auto flight ability of the miniature unmanned helicopter, strengthen system reliability, expand the application range of the unmanned helicopter and enable the helicopter to complete given missions beyond the visual range.

Description

technical field [0001] The invention relates to a control technology of an aircraft, in particular to an autonomous flight control system of a small unmanned helicopter. technical background [0002] With the development of autonomous control technology, unmanned aerial vehicle (UAV, Unmanned Aerial Vehicle) has begun extensive research all over the world. Unmanned helicopters have many advantages that unmanned fixed-wing aircraft do not have, and have unique flight performance and use value. It has no casualties, small size, low cost, and strong battlefield survivability; in terms of military use, unmanned helicopters can not only perform various non-lethal tasks, but also perform various soft and hard lethal tasks, including reconnaissance, surveillance, target Interception, bait, attack, communication relay, etc.; in terms of civilian use, unmanned helicopters have broad application prospects in aerial photography, atmospheric monitoring, traffic monitoring, resource exp...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G05D1/08G05D1/10G05D1/00G05B19/418
CPCY02P90/02
Inventor 韩建达齐俊桐姜哲赵新刚
Owner SHENYANG INST OF AUTOMATION - CHINESE ACAD OF SCI
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