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基于CAN總線(xiàn)控制系統的航天特種機械臂設計
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北京航天發(fā)射技術(shù)研究所

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Design of aerospace special manipulator based on CAN bus control system
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    摘要:

    航天特種機械臂具備精確操作和視覺(jué)識別的能力,在載人航天領(lǐng)域中廣泛應用,為了在復雜環(huán)境中精準完成陸基裝配任務(wù),設計基于CAN總線(xiàn)控制系統的航天特種機械臂。從關(guān)節、連桿、驅動(dòng)電機、鎖緊制動(dòng)器等方面,組裝航天特種機械臂結構元件。裝設航天特種機械臂控制器,在控制器中加設一個(gè)串行通信接口,將控制器連接到CAN總線(xiàn)中,配置CAN總線(xiàn)控制系統的通信協(xié)議,完成航天特種機械臂硬件結構設計。利用航天特種機械臂中傳感器設備,檢測航天特種機械臂實(shí)時(shí)位姿,補償航天特種機械臂重力負載。根據機械臂工作任務(wù),規劃移動(dòng)軌跡,在控制器的支持下,通過(guò)控制量的計算與通信,實(shí)現航天特種機械臂的控制功能。性能測試實(shí)驗表明,設計基于CAN總線(xiàn)控制系統的航天特種機械臂平均位置和關(guān)節姿態(tài)角的控制誤差分別為3.0m和0.32°,平均形變量為2.64m2,具有較好的控制性能和抗壓性能。

    Abstract:

    The space special manipulator has the ability of precise operation and visual recognition, and is widely used in the field of manned spaceflight. In order to accurately complete space tasks in complex environments, the space special manipulator based on CAN bus control system is designed. The structural elements of the special space manipulator are assembled from the aspects of joints, connecting rods, drive motors and locking brakes. The controller of aerospace special manipulator is installed, a serial communication interface is added in the controller, the controller is connected to the CAN bus, the communication protocol of the CAN bus control system is configured, and the hardware structure design of aerospace special manipulator is completed. The real-time position and attitude of the space special manipulator are detected by the sensor equipment in the space special manipulator, and the gravity load of the space special manipulator is compensated. According to the work task of the manipulator, the movement trajectory is planned. With the support of the controller, the control function of the space special manipulator is realized through the calculation and communication of the control quantity. The performance test results show that the control errors of the average position and joint attitude angle of the space special manipulator designed based on the CAN bus control system are 3.0m and 0.32 ° respectively, and the average shape variable is 2.64m2, which has good control performance and compression resistance.

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王博,鄧鵬程,劉國英,馮超,毛利民.基于CAN總線(xiàn)控制系統的航天特種機械臂設計計算機測量與控制[J].,2023,31(5):114-119.

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歷史
  • 收稿日期:2022-09-20
  • 最后修改日期:2022-10-25
  • 錄用日期:2022-10-25
  • 在線(xiàn)發(fā)布日期: 2023-05-19
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