中国空间科学技术
中國空間科學技術
중국공간과학기술
CHINESE SPACE SCIENCE AND TECHNOLOGY
2010年
1期
1-9
,共9页
自主时间同步%铷原子时钟%钟差预报%Hadamard方差%卡尔曼滤波%导航卫星
自主時間同步%銣原子時鐘%鐘差預報%Hadamard方差%卡爾曼濾波%導航衛星
자주시간동보%여원자시종%종차예보%Hadamard방차%잡이만려파%도항위성
Auto-time synchronization%Rubidium atomic frequency standards%Clock error prediction%Hadamard variance%Kalman filter%Navigation satellite
文章在总结国内外研究成果基础上,针对GPS铷钟虽然短期稳定性较好,但采用Allan方差描述铷钟频率稳定性时,其钟差状态方程仅为两参数,在较长平滑时间里存在时钟漂移和甚低频噪声的影响,使噪声特性淹没或估值不收敛的缺陷,引入Hadamard方差建立了三参数系统状态误差模型,通过三次采样方差从模型上解决了线形漂移和甚低频噪声的影响问题.在时钟系统状态模型和星间双向测量方程建模基础上,给出了工程实用的标准Kalman基本滤波方程.数值分析仿真表明,采用Hadamard方差描述时钟频率稳定性显著提高星载时钟自主同步精度,从而克服了Allan方差描述产生的频率漂移影响较大和甚低频噪声不收敛的问题.
文章在總結國內外研究成果基礎上,針對GPS銣鐘雖然短期穩定性較好,但採用Allan方差描述銣鐘頻率穩定性時,其鐘差狀態方程僅為兩參數,在較長平滑時間裏存在時鐘漂移和甚低頻譟聲的影響,使譟聲特性淹沒或估值不收斂的缺陷,引入Hadamard方差建立瞭三參數繫統狀態誤差模型,通過三次採樣方差從模型上解決瞭線形漂移和甚低頻譟聲的影響問題.在時鐘繫統狀態模型和星間雙嚮測量方程建模基礎上,給齣瞭工程實用的標準Kalman基本濾波方程.數值分析倣真錶明,採用Hadamard方差描述時鐘頻率穩定性顯著提高星載時鐘自主同步精度,從而剋服瞭Allan方差描述產生的頻率漂移影響較大和甚低頻譟聲不收斂的問題.
문장재총결국내외연구성과기출상,침대GPS여종수연단기은정성교호,단채용Allan방차묘술여종빈솔은정성시,기종차상태방정부위량삼수,재교장평활시간리존재시종표이화심저빈조성적영향,사조성특성엄몰혹고치불수렴적결함,인입Hadamard방차건립료삼삼수계통상태오차모형,통과삼차채양방차종모형상해결료선형표이화심저빈조성적영향문제.재시종계통상태모형화성간쌍향측량방정건모기출상,급출료공정실용적표준Kalman기본려파방정.수치분석방진표명,채용Hadamard방차묘술시종빈솔은정성현저제고성재시종자주동보정도,종이극복료Allan방차묘술산생적빈솔표이영향교대화심저빈조성불수렴적문제.
High-accuracy auto-time synchronization is the foundation of the navigation constellation and a key technology of auto-navigation. The accuracy of time synchronization among navigation satellites is directly affected by frequency stability of on-board atomic clocks. GPS Rubidium atomic frequency standards (RAFS) exhibit non-trivial aging and aging noise characteristics, whereas the Allan variance does not explicitly converge for the noise type of α not more than-3), and can be greatly affected by frequency drift. The three-sample variance, commonly referred as a renormalized Hadamard variance was proposed, which was unaffected by linear frequency drift, converges for α more than-5), and thus can be used for modeling noise in Rubidium frequency standards. A standard Kalman filter algorithm based on improved clock error predication model and inter-satellites measurements equations was established for practical use in on-board RAFS. System simulation results show that more precise auto-time synchronization is achieved by this method.