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作 者:刘宪阳[1] 金根 董启甲[1] 单建丰 董娟娟[1] LIU Xianyang;JIN Gen;DONG Qijia;SHAN Jianfeng;DONG Juanjuan(Space Star Technology Co.,Ltd.,Beijing 100086,China;Tianjin Zhongwei Aerospace Data System Technology Co.,Ltd.,Tianjin 300462,China)
机构地区:[1]航天恒星科技有限公司,北京100086 [2]天津航天中为数据系统科技有限公司,天津300462
出 处:《导航定位学报》2021年第4期131-136,共6页Journal of Navigation and Positioning
摘 要:针对由于单点定位精度较低,难以引导飞行器进场着陆的问题,提出一种飞行器着陆的引导方法:利用北斗卫星导航系统(BDS)伪距差分定位数据来引导飞行器着陆;并建立BDS伪距差分定位模拟环境。实验结果表明,在短基线情况下,BDS伪距实时差分定位的位置精度小于1 m,证明了BDS伪距差分定位技术用于引导飞行器进场着陆的有效性。Aiming at the problem that due to the low accuracy of single point positioning,it is difficult to guide aircrafts in approach and landing,the paper proposed a guiding method for aircraft landing:pseudo range differential positioning data of Beidou navigation satellite system(BDS)were used to guide the landing;and the simulation environment of Beidou pseudo range differential positioning was established.Experimental result showed that the position accuracy of real-time Beidou pseudo range differential positioning would be less than 1 m in the case of short baselines,which could prove the feasibility of the proposed method.
分 类 号:P228[天文地球—大地测量学与测量工程]
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