ATTITUDE-CONTROL OF A SPINNING SKYLAB

被引：0

作者：

SELTZER, SM

SCHWEITZER, G

ASNER, B

机构：

[1] NASA, MARSHALL SPACE FLIGHT CTR, ASTRION LAB, HUNTSVILLE, AL 35801 USA

[2] TECH UNIV MUNICH, INST B MECH, MUNICH, WEST GERMANY

[3] BOGAZICI UNIV, MATH DEPT, ISTANBUL, TURKEY

来源：

JOURNAL OF SPACECRAFT AND ROCKETS | 1973年 / 10卷 / 03期

关键词：

D O I：

10.2514/3.61869

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：200 / 207

页数：8

共 50 条

[1] SKYLAB ATTITUDE-CONTROL SYSTEM
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IRBY, JE
[J]. IBM JOURNAL OF RESEARCH AND DEVELOPMENT, 1976, 20 (01) : 58 - 66
[2] ATTITUDE-CONTROL OF SPINNING SPACECRAFT BY RADIATION PRESSURE
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[J]. JOURNAL OF SPACECRAFT AND ROCKETS, 1976, 13 (12) : 765 - 766
[3] PERIODIC ATTITUDE-CONTROL OF A SLOWLY SPINNING SPACECRAFT
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[J]. JOURNAL OF SPACECRAFT AND ROCKETS, 1973, 10 (11) : 716 - 723
[4] GEOMAGNETIC ATTITUDE-CONTROL OF AN AXISYMMETRIC SPINNING SATELLITE
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[J]. JOURNAL OF SPACECRAFT AND ROCKETS, 1972, 9 (06) : 391 - +
[5] MFDS OF SPINNING SATELLITE AND ATTITUDE-CONTROL USING GYROTORQUERS
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[J]. IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, 1989, 25 (05) : 611 - 620
[6] TIME-OPTIMAL ATTITUDE-CONTROL SCHEME FOR A SPINNING MISSILE
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[7] ACTIVE ATTITUDE-CONTROL OF A SPINNING SYMMETRICAL SATELLITE IN AN ELLIPTIC ORBIT
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[J]. JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1983, 6 (04) : 315 - 320
[8] RATIONAL FRACTION APPROACH AND ATTITUDE-CONTROL OF SPINNING SATELLITE USING GYROTORQUER
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[J]. PROCEEDINGS OF THE 1989 AMERICAN CONTROL CONFERENCE, VOLS 1-3, 1989, : 1579 - 1584
[9] STABLE FRACTION APPROACH AND ATTITUDE-CONTROL OF A SPINNING SATELLITE USING A GYROTORQUER
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[J]. INTERNATIONAL JOURNAL OF SYSTEMS SCIENCE, 1992, 23 (03) : 311 - 328
[10] THE ATTITUDE-CONTROL PROBLEM
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[J]. IEEE TRANSACTIONS ON AUTOMATIC CONTROL, 1991, 36 (10) : 1148 - 1162

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