本文關(guān)鍵詞： 衛(wèi)星信號 實驗平臺 飛行軌跡 模擬 導(dǎo)航精度　出處：《空間電子技術(shù)》2016年05期 　論文類型：期刊論文

【摘要】：基于對低空低速飛機飛行軌跡的分析,利用搭建的北斗信號實驗平臺模擬實現(xiàn)了飛行過程中對飛機位置及其速度的測算,并用以分析衛(wèi)星信號接收機的定位誤差。通過實驗接收信號解碼并解析NMEA語句,對比軌跡運動方程和實際接收的數(shù)據(jù)軌跡來分析導(dǎo)航精度。經(jīng)驗證,該方法可實際應(yīng)用于對安裝在飛機上的接收機進行重復(fù)性的精度測試實驗分析,通過對真實環(huán)境中誤差影響因素的再現(xiàn),以及反復(fù)實現(xiàn)不同動態(tài)的軌跡來進行實驗測試及精度分析,節(jié)省直接實測過程中投入的人力和設(shè)備以及時間成本。
[Abstract]:Analysis of low speed and low altitude flight path based on simulation to calculate the position and speed of the aircraft during flight by Beidou signal experimental platform, and used to analysis positioning satellite signal receiver error. By decoding the received signal and experimental analysis of NMEA statements, analysis of navigation accuracy comparison of trajectory equation and the actual data received track. After verification, the method can be applied to the analysis of the precision testing experiment was repeated on the receiver mounted on the aircraft, the factors which influence on reproduction error in real environment, and repeatedly achieve different dynamic trajectories to measuring accuracy, save direct measurement process manpower and equipment time and cost.

【作者單位】： 中國民航飛行學(xué)院空中交通管理學(xué)院;東海航空有限公司;
【分類號】：TN967.1

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1 金宏,張洪鉞,金忠;導(dǎo)航精度的評估與檢驗[J];航空學(xué)報;1997年02期

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本文編號：1501726