遠程遙測姿態(tài)控制系統設計

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遠程遙測姿態(tài)控制系統設計
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作者單位:(1.中北大學(xué) 電子測試技術(shù)重點(diǎn)實(shí)驗室,太原 030051;;2.中北大學(xué) 儀器科學(xué)與動(dòng)態(tài)測試教育部重點(diǎn)實(shí)驗室,太原 030051;;3.中國運載火箭技術(shù)研究院,北京 100076)
作者簡(jiǎn)介:張鳳英(1990-),女,碩士研究生,主要從事自動(dòng)測試與控制技術(shù)方向的研究。 劉文怡(1970-),男,博士,教授,博導,主要從事網(wǎng)絡(luò )操作系統和微系統集成技術(shù)方向的研究。[FQ)]
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Design of Telemetry Posture Control System

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(1.Lab. of Science and Technology on Electronic Test & Measurement, North China University, Taiyuan 030051, China;2.Ministerial Key Laboratory of Instrumentation Science & Dynamic Measurement North China University, Taiyuan 030051, China;3.China Academy of Launch Vehicle Technology,Beijing 100076,China)[JZ)]

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摘要:

為全面測控飛行器姿態(tài),設計了一種能實(shí)時(shí)監測、控制飛行器姿態(tài)傾角的遠程遙測系統；采用FPGA進(jìn)行中央邏輯控制,構建了智能變送模塊；將上位機作為終端設備,結合步進(jìn)電機24BYJ48-5V與雙軸傾角傳感器ROB100等前端設備,經(jīng)過(guò)硬件及軟件調試,完成步進(jìn)電機閉環(huán)控制,實(shí)現-90°～+90°范圍內對飛行器任意傾角值的實(shí)時(shí)測量與控制,測試精度達0.5°；通過(guò)大量試驗結果及分析表明,該系統可靠性高、可移植性強,能夠完成對飛行器姿態(tài)的實(shí)時(shí)測控,各項性能指標均滿(mǎn)足項目需求。

Abstract:

Aimed at test the posture of aircraft roundly, designed a telemetry system which can real-time monitor and control the posture angle of aircraft. The logic control of this system was completed by FPGA, formed a smart transmitting module. Used the host computer as terminal device, combining the front device like stepping motor 24BYJ48-5V and tilt sensor ROB100, through debugging of hardware and software completed stepping motor close loop control . Real-time measurement and control of any aircraft angle between -90° to +90° are implemented, and the measurement precision can achieve 0.5°. The abundant experimental and analysis proved that, this system has the advantages of reliability and easy expansion, it can complete the real-time test of aircraft,which meets the requirement of various function index.

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張鳳英,劉文怡,楊慧,馬睿.遠程遙測姿態(tài)控制系統設計計算機測量與控制[J].,2015,23(1):102-105.

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在線(xiàn)發(fā)布日期: 2015-03-27
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