On-vehicle computer software system of miniature unmanned aerial vehicle

A technology of airborne computer and small UAV, applied in the direction of control/adjustment system, non-electric variable control, instrument, etc., can solve the problems of UAV limitation and limited size, achieve good reliability, reduce burden, The effect of strong versatility

A technology of airborne computer and small UAV, applied in the direction of control/adjustment system, non-electric variable control, instrument, etc., can solve the problems of UAV limitation and limited size, achieve good reliability, reduce burden, The effect of strong versatility

CN105867412AInactive Publication Date: 2016-08-17平玉兰

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  • On-vehicle computer software system of miniature unmanned aerial vehicle
  • On-vehicle computer software system of miniature unmanned aerial vehicle
  • On-vehicle computer software system of miniature unmanned aerial vehicle

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Embodiment Construction

[0018] refer to Figure 1 to Figure 3 , the present invention designs a kind of airborne computer software system of small unmanned aerial vehicle, comprises airborne computer, and described airborne computer connects airborne data acquisition system, flight control system, navigation system and storage system through RS-232 interface; The software system of the airborne computer is divided into driver layer, data processing layer, control layer and application layer;

[0019] The driver layer is responsible for the collection of sensor data, the reading of data transmission communication data, the collection of combined navigation raw data and the control work of the actuator; the data processing layer calls the driver layer module to obtain raw data, decodes the raw data and Transformation, release the processed data to the control layer; the data required by the control layer depends on the data processing layer, and interface data coupling is performed through the object r...

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Abstract

The invention discloses an airborne computer software system for a small unmanned aerial vehicle, comprising an airborne computer, the airborne computer is connected to an airborne data acquisition system, a flight control system, a navigation system and a storage system through an RS‑232 interface; The software system of the airborne computer is divided into driver layer, data processing layer, control layer and application layer; adopting the method of layered design, through the layer division and task division of functional modules, the embedded system with high real-time and high reliability Based on the real-time multi-task operating system, the multi-task concurrency design is completed, and the highly scalable software system architecture is determined. The introduction of the data-centered system inter-process communication method increases the reliability and flexibility of the data communication of the software system, enhances the real-time performance of the flight control system to collect analog data, reduces the burden on the flight control computer CPU, and improves the The overall parallel processing capability of the flight control system.

Description

technical field [0001] The invention relates to the technical field of unmanned aerial vehicle control, in particular to an onboard computer software system of a small unmanned aerial vehicle. Background technique [0002] With the development of new technologies and new equipment, the development of drones is also accelerating, and various drones have come out one after another. Due to the advantages of UAVs such as maneuverability, small size, low cost, and no casualties, the research and development of UAVs has been highly valued by many countries. In the military, UAVs can be used as aerial reconnaissance platforms and weapon platforms. By carrying different equipment, they can perform tasks such as reconnaissance and surveillance, ground attack, electronic interference, communication relay, target positioning, and effective assessment of attack damage. In terms of civilian use, UAVs are also promising. It can be used in aerial photography, meteorological detection, sur...

Claims

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Application Information

Patent Timeline
17 Aug 2016
Publication
CN105867412A
IPC
G05D1/10
CPC
G05D1/101
Inventors
不公告发明人