MEASUREMENT OF THE PASSIVE ATTITUDE-CONTROL PERFORMANCE OF A RECOVERED SPACECRAFT

被引:3
作者
GREGORY, JC [1 ]
PETERS, PN [1 ]
机构
[1] NASA,GEORGE C MARSHALL SPACE FLIGHT CTR,SPACE SCI LAB,HUNTSVILLE,AL 35812
基金
美国国家科学基金会;
关键词
D O I
10.2514/3.20834
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
[No abstract available]
引用
收藏
页码:282 / 284
页数:3
相关论文
共 50 条
[41]   DETERMINATION OF POLES AND ZEROS OF TRANSFER-FUNCTIONS FOR FLEXIBLE SPACECRAFT ATTITUDE-CONTROL [J].
OHKAMI, Y ;
LIKINS, PW .
INTERNATIONAL JOURNAL OF CONTROL, 1976, 24 (01) :13-22
[42]   SYNTHESIS AND DEVELOPMENT PROCEDURE OF MICROPROCESSOR SOFTWARE PROGRAM FOR SPACECRAFT DIGITAL ATTITUDE-CONTROL [J].
KIDA, T ;
OKAMOTO, O ;
OHKAMI, Y .
TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, 1979, 21 (54) :173-181
[43]   OPTIMAL SOLAR PRESSURE ATTITUDE-CONTROL OF SPACECRAFT .1. INERTIALLY-FIXED ATTITUDE STABILIZATION [J].
PANDE, KC ;
VENKATACHALAM, R .
ACTA ASTRONAUTICA, 1982, 9 (09) :533-540
[44]   SPACECRAFT ATTITUDE-CONTROL AND STABILIZATION - APPLICATIONS OF GEOMETRIC CONTROL-THEORY TO RIGID BODY MODELS [J].
CROUCH, PE .
IEEE TRANSACTIONS ON AUTOMATIC CONTROL, 1984, 29 (04) :321-331
[45]   OPTIMAL SOLAR PRESSURE ATTITUDE-CONTROL OF SPACECRAFT .2. LARGE-ANGLE ATTITUDE MANEUVERS [J].
VENKATACHALAM, R ;
PANDE, KC .
ACTA ASTRONAUTICA, 1982, 9 (09) :541-545
[46]   Modeling of Microaccelerations Caused by Running of Attitude-Control Engines of Spacecraft with Elastic Structural Elements [J].
A. V. Sedelnikov .
Microgravity Science and Technology, 2016, 28 :491-498
[47]   THE ATTITUDE-CONTROL PROBLEM - COMMENTS [J].
FJELLSTAD, OE ;
FOSSEN, TI .
IEEE TRANSACTIONS ON AUTOMATIC CONTROL, 1994, 39 (03) :699-700
[48]   SKYLAB ATTITUDE-CONTROL SYSTEM [J].
COON, TR ;
IRBY, JE .
IBM JOURNAL OF RESEARCH AND DEVELOPMENT, 1976, 20 (01) :58-66
[49]   A MAGNETIC ATTITUDE-CONTROL SYSTEM FOR PRECISION POINTING OF THE ROLLING GP-B SPACECRAFT [J].
PARKINSON, BW ;
KASDIN, NJ .
ACTA ASTRONAUTICA, 1990, 21 (6-7) :477-486