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基于姿態(tài)隨動(dòng)技術(shù)的直升機低高度測量
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中國飛行試驗研究院,中國飛行試驗研究院,

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Helicopter low altitude measurement based onattitude following technology
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    摘要:

    在飛行試驗中懸停性能是直升機性能的重要試飛科目。該科目科研試飛鑒定要求有大量的樣本數據(海拔、溫度、重量、構形的組合)以獲取比較準確的試驗結論。其中,離地高度是懸停科目試飛與小速度科目試飛中的關(guān)鍵參數。直升機的低高度信息通常由氣壓式高度傳感器、無(wú)線(xiàn)電高度表獲取。由于受到地面效應、姿態(tài)、風(fēng)速風(fēng)向等諸多因素的干擾,從而無(wú)法保證高精度和可靠性。激光測距逐漸成為一種先進(jìn)的測量手段應用于直升機低高度測量中。但是在具體實(shí)施過(guò)程中由于直升機機動(dòng)飛行姿態(tài)變化導致激光高度測量的誤差增大與失效。通過(guò)機載姿態(tài)跟隨技術(shù)研究不僅克服了直升機機動(dòng)狀態(tài)下姿態(tài)變化引起的低高度測量誤差與失效,而且可由機載綜合采集系統將低高度數據融合,實(shí)時(shí)發(fā)送給地面站遙測接收與存儲,可以極大擴充數據樣本,從而獲取比較準確的試驗結論。

    Abstract:

    In flight test, hovering performance is an important test subject for helicopter performance. The scientific research flight test of this subject requires a large number of sample data (altitude, temperature, weight, configuration combination) to get more accurate test conclusions. Among them, the ground height is the key parameter of hover test and small speed flight test. Low altitude information of helicopter is usually obtained by air pressure height sensor and radio altimeter. Due to many disturbances such as ground effect, posture, wind speed and wind direction, the high accuracy and reliability can,t be guaranteed. Laser ranging has gradually become an advanced measurement method for helicopter low altitude measurement. But in the specific implementation process, the error of laser height measurement increases and fails due to the change of helicopter maneuvering flight attitude. The airborne attitude follow technology not only overcomes the low altitude measurement error and failure caused by the attitude change in the helicopter"s maneuver state, but also combines the low altitude data by the airborne integrated acquisition system and sends it to the ground station telemetry receiving and storage in real time. It can greatly expand the data samples and obtain more accurate data. The conclusion of the test.

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馬亞平,劉 鵬,谷士鵬.基于姿態(tài)隨動(dòng)技術(shù)的直升機低高度測量計算機測量與控制[J].,2018,26(8):27-30.

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歷史
  • 收稿日期:2018-05-14
  • 最后修改日期:2018-06-18
  • 錄用日期:2018-06-19
  • 在線(xiàn)發(fā)布日期: 2018-09-04
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