ESTIMATION OF LOCAL VERTICAL AND ORBITAL PARAMETERS FOR AN EARTH SATELLITE USING HORIZON SENSOR MEASUREMENTS

被引：9

作者：

KNOLL, AL

EDELSTEI.MM

机构：

来源：

关键词：

D O I：

10.2514/3.2851

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：338 / &

共 16 条

[1] ASTROM JK, 1962, RJ222 IBM RES REP, P19
[2] Battin R. H., 1964, ASTRONAUTICAL GUIDAN, P338
[3] A STATISTICAL OPTIMIZING NAVIGATION PROCEDURE FOR SPACE FLIGHT
BATTIN, RH
[J]. ARS JOURNAL, 1962, 32 (11): : 1681 - 1696
[4] BROUWER, 1961, METHODS CELESTIAL ME, P77
[5] DANBY JMA, 1962, FUNDAMENTALS CELESTI, P261
[6] SELF-CONTAINED SATELLITE NAVIGATION SYSTEMS
FRAZIER, M
KRIEGSMAN, B
NESLINE, FW
[J]. AIAA JOURNAL, 1963, 1 (10) : 2310 - 2316
[7] HO YC, 1964, P JOINT AUTOM CONTRO, P382
[8] HO YC, 1964, I ELEC ELECTRON ENGR, VAC 9
[9] Ho Yu Chi, 1963, J MATH ANAL APPL, V6, P152
[10] CELESTIAL RATE SENSING
KARRENBERG, HK
ROBERSON, RE
[J]. ARS JOURNAL, 1961, 31 (03): : 440 - 441