电光与控制
電光與控製
전광여공제
ELECTRONICS OPTICS & CONTROL
2014年
12期
25-29
,共5页
飞行控制系统%飞行员诱发振荡%带宽准则%平均相位速率准则%过渡滞后
飛行控製繫統%飛行員誘髮振盪%帶寬準則%平均相位速率準則%過渡滯後
비행공제계통%비행원유발진탕%대관준칙%평균상위속솔준칙%과도체후
flight control systems%pilot induced oscillation%bandwidth criterion%phase rate criterion%excessive lag
针对飞机过度滞后会导致飞行员诱发振荡的问题,提出综合运用频域法和时域法对过度滞后与飞行员诱发振荡间的关系进行定量研究。建立了简化的人机闭环系统模型,分析了人机闭环系统不稳定的充要条件。频域内应用伯德图和尼柯尔斯图对有效飞机频域特性进行了分析,通过带宽准则和平均相位速率准则对有效时延与飞行员诱发振荡间的关系进行定量评估。时域内运用飞机的飞行员诱发振荡时间历程曲线及延迟时间与飞行品质评分间关系曲线,对过度滞后的影响进行了定量研究。研究结果可为控制飞机的过度滞后提供定量依据。
針對飛機過度滯後會導緻飛行員誘髮振盪的問題,提齣綜閤運用頻域法和時域法對過度滯後與飛行員誘髮振盪間的關繫進行定量研究。建立瞭簡化的人機閉環繫統模型,分析瞭人機閉環繫統不穩定的充要條件。頻域內應用伯德圖和尼柯爾斯圖對有效飛機頻域特性進行瞭分析,通過帶寬準則和平均相位速率準則對有效時延與飛行員誘髮振盪間的關繫進行定量評估。時域內運用飛機的飛行員誘髮振盪時間歷程麯線及延遲時間與飛行品質評分間關繫麯線,對過度滯後的影響進行瞭定量研究。研究結果可為控製飛機的過度滯後提供定量依據。
침대비궤과도체후회도치비행원유발진탕적문제,제출종합운용빈역법화시역법대과도체후여비행원유발진탕간적관계진행정량연구。건립료간화적인궤폐배계통모형,분석료인궤폐배계통불은정적충요조건。빈역내응용백덕도화니가이사도대유효비궤빈역특성진행료분석,통과대관준칙화평균상위속솔준칙대유효시연여비행원유발진탕간적관계진행정량평고。시역내운용비궤적비행원유발진탕시간역정곡선급연지시간여비행품질평분간관계곡선,대과도체후적영향진행료정량연구。연구결과가위공제비궤적과도체후제공정량의거。
Excessive lags of aircraft could cause Pilot Induced Oscillations(PIO).The frequency domain method and time domain method were used combinedly for studying the relationship between excessive lags and PIO quantitatively.A simplified closed-loop aircraft-pilot system model was built up,and the aircraft-pilot system stability was analyzed.In frequency domain,the frequency characteristic of effective aircraft was investigated by using Bode plot and Nichols plot,and quantitative estimation was made to the relation of the effective time delay and PIO by using bandwidth criterion and phase rate criterion.In time domain,the influence of excessive lags was quantitatively studied by using pilot induced oscillations time history and pilot rating.The results can provide a quantitative reference for controlling excessive lags of aircraft.