北京航空航天大学学报
北京航空航天大學學報
북경항공항천대학학보
2001年
2期
161-163
,共3页
卫星导航%可靠性%故障检测%全球定位系统%完整性
衛星導航%可靠性%故障檢測%全毬定位繫統%完整性
위성도항%가고성%고장검측%전구정위계통%완정성
对伪距残差最小二乘的接收机自主完整性监测(RAIM)算法进行了分析.在此基础上,通过对接收机时钟偏差的建模,将模型预测的时钟偏差引入伪距残差最小二乘的RAIM算法中,保证了在可见星仅为4颗的情况下,仍能利用χ2检验法对全球定位系统(GPS)进行完整性监测,从而达到提高完整性监测算法有效性的目的.计算机仿真的结果显示,这种辅助方式不仅计算简单,而且有效可行.
對偽距殘差最小二乘的接收機自主完整性鑑測(RAIM)算法進行瞭分析.在此基礎上,通過對接收機時鐘偏差的建模,將模型預測的時鐘偏差引入偽距殘差最小二乘的RAIM算法中,保證瞭在可見星僅為4顆的情況下,仍能利用χ2檢驗法對全毬定位繫統(GPS)進行完整性鑑測,從而達到提高完整性鑑測算法有效性的目的.計算機倣真的結果顯示,這種輔助方式不僅計算簡單,而且有效可行.
대위거잔차최소이승적접수궤자주완정성감측(RAIM)산법진행료분석.재차기출상,통과대접수궤시종편차적건모,장모형예측적시종편차인입위거잔차최소이승적RAIM산법중,보증료재가견성부위4과적정황하,잉능이용χ2검험법대전구정위계통(GPS)진행완정성감측,종이체도제고완정성감측산법유효성적목적.계산궤방진적결과현시,저충보조방식불부계산간단,이차유효가행.
The characters of least-squares-residuals method belonging to receiver autonomous integrity monitoring(RAIM) were analyzed. After the receiver clock bias behavior was accurately modeled using global positioning system(GPS) measurements, a new algorithm for RAIM was developed based on the least-squares-residuals method with the aiding of receiver clock bias. It can be gained through the model. The novelty lies in that on the condition of only four satellites in view, it can still use chi-square distribution to detect the failure satellite of GPS. So it can improve the availability of RAIM. The simulation results show that this algorithm is not only simple but also available and feasible.