ESTIMATION OF LOCAL ATTITUDE OF ORBITING SPACECRAFT

[1] [Anonymous], 1968, FILTERING STOCHASTIC

[2] ASTHEIMER RW, 1969, SEP SPAC ATT DET S

[3] ASTHEIMER RW, 1971, AUTOMATICA

[4] Battin R. H., 1964, ASTRONAUTICAL GUIDAN

[5] A PASSIVE SYSTEM FOR DETERMINING THE ATTITUDE OF A SATELLITE [J]. AIAA JOURNAL, 1964, 2 (07) : 1350 - 1351

[6] BOWERS JL, 1968, AIAA J SPACECRAFT RO, V5, P903

[7] BROCK LD, 1965, THESIS MIT

[8] BRYSON A, 1969, APPLIED OPTIMAL CONT

[9] ALIGNMENT OF INERTIAL GUIDANCE SYSTEMS BY GYROCOMPASSING-LINEAR THEORY [J]. JOURNAL OF THE AEROSPACE SCIENCES, 1961, 28 (11): : 885 - &

[10] CARROLL JE, 1969, SEP SPAC ATT DET S

[1] [Anonymous], 1968, FILTERING STOCHASTIC

[2] ASTHEIMER RW, 1969, SEP SPAC ATT DET S

[3] ASTHEIMER RW, 1971, AUTOMATICA

[4] Battin R. H., 1964, ASTRONAUTICAL GUIDAN

[5] A PASSIVE SYSTEM FOR DETERMINING THE ATTITUDE OF A SATELLITE [J]. AIAA JOURNAL, 1964, 2 (07) : 1350 - 1351

[6] BOWERS JL, 1968, AIAA J SPACECRAFT RO, V5, P903

[7] BROCK LD, 1965, THESIS MIT

[8] BRYSON A, 1969, APPLIED OPTIMAL CONT

[9] ALIGNMENT OF INERTIAL GUIDANCE SYSTEMS BY GYROCOMPASSING-LINEAR THEORY [J]. JOURNAL OF THE AEROSPACE SCIENCES, 1961, 28 (11): : 885 - &

[10] CARROLL JE, 1969, SEP SPAC ATT DET S