VIBRATION OF A ROTATING UNIFORM BEAM .1. ORIENTATION IN THE AXIS OF ROTATION

[1] BAUER HF, 1976, RAUMFAHRTFORSCHUNG, V20, P165

[2] EXPLANATION OF ANOMALOUS SPIN BEHAVIOR OF SATELLITES WITH LONG FLEXIBLE ANTENNAE [J]. JOURNAL OF SPACECRAFT AND ROCKETS, 1967, 4 (09) : 1139 - &

[3] INFLUENCE OF FLEXIBLE APPENDAGES ON DUAL-SPIN SPACECRAFT DYNAMICS AND CONTROL [J]. JOURNAL OF SPACECRAFT AND ROCKETS, 1970, 7 (09) : 1049 - &

[4] EQUATIONS OF MOTION OF FLEXIBLE SPACECRAFT [J]. JOURNAL OF SPACECRAFT AND ROCKETS, 1971, 8 (06) : 561 - &

[5] HUGHES PC, 1971, CELESTIAL MECH, V4, P295

[6] KEAT JE, 1973, J SPACECRAFT ROCKETS, V10, P94

[7] Likins P.W., 1972, INT J SOLIDS STRUCT, V8, P709, DOI 10.1016/0020-7683(72)90038-8

[8] LIKINS PW, 1971, J SPACECRAFT ROCKETS, V8, P264, DOI 10.2514/3.30258

[9] MATHEMATICAL MODELING OF SPINNING ELASTIC BODIES FOR MODAL ANALYSIS [J]. AIAA JOURNAL, 1973, 11 (09) : 1251 - 1258

[10] LIKINS PW, 1971, ASTRONAUT AERONAUT, V9, P64

[1] BAUER HF, 1976, RAUMFAHRTFORSCHUNG, V20, P165

[2] EXPLANATION OF ANOMALOUS SPIN BEHAVIOR OF SATELLITES WITH LONG FLEXIBLE ANTENNAE [J]. JOURNAL OF SPACECRAFT AND ROCKETS, 1967, 4 (09) : 1139 - &

[3] INFLUENCE OF FLEXIBLE APPENDAGES ON DUAL-SPIN SPACECRAFT DYNAMICS AND CONTROL [J]. JOURNAL OF SPACECRAFT AND ROCKETS, 1970, 7 (09) : 1049 - &

[4] EQUATIONS OF MOTION OF FLEXIBLE SPACECRAFT [J]. JOURNAL OF SPACECRAFT AND ROCKETS, 1971, 8 (06) : 561 - &

[5] HUGHES PC, 1971, CELESTIAL MECH, V4, P295

[6] KEAT JE, 1973, J SPACECRAFT ROCKETS, V10, P94

[7] Likins P.W., 1972, INT J SOLIDS STRUCT, V8, P709, DOI 10.1016/0020-7683(72)90038-8

[8] LIKINS PW, 1971, J SPACECRAFT ROCKETS, V8, P264, DOI 10.2514/3.30258

[9] MATHEMATICAL MODELING OF SPINNING ELASTIC BODIES FOR MODAL ANALYSIS [J]. AIAA JOURNAL, 1973, 11 (09) : 1251 - 1258

[10] LIKINS PW, 1971, ASTRONAUT AERONAUT, V9, P64