Eigenaxis Maneuver Strategy with Input Shaping for Three-axis Maneuver of Flexible Spacecrafts

来源 :第八届工业与应用数学国际大会 | 被引量 : 0次 | 上传用户:SuperXF
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  An eigenaxis maneuver strategy of flexible spacecraft with vibration suppression is investigated.The eigenaxis maneuver is realized by sliding mode methodology so that three-axis attitude maneuver can be treated as single-axis attitude motion around the eigenaxis.
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