DocumentCode :
3454505
Title :
Modeling of impact dynamics and impulse minimization for space robots
Author :
Yoshida, Kazuya ; Sashida, Naoki
Author_Institution :
Dept. of Mech. & Aerosp. Eng., Tokyo Inst. of Technol., Japan
Volume :
3
fYear :
1993
fDate :
26-30 Jul 1993
Firstpage :
2064
Abstract :
Investigates impact dynamics among free-floating multibody systems in space, by developing an extended inertial tensor concept, and establishes the theoretical basis for floating chain collisions. The authors have developed a concept named an `extended inversed inertia tensor´ (Ex-IIT), paying attention to free-floating behavior in the space environment. They apply Ex-IIT to impulse minimization arguments. To illustrate the magnitude of the impulses caused by link collisions in various conditions, the concepts of `impulse index´ and `impulse ellipsoid´ are introduced. By means of these concepts, the authors discuss the relationship of the impulse to collision directions and link postures, in order to determine the condition minimizing the impulse
Keywords :
aerospace control; Ex-IIT; collision directions; extended inversed inertia tensor; floating chain collisions; free-floating multibody systems; impact dynamics; impulse ellipsoid; impulse index; impulse minimization; link collisions; link postures; space robots; Aerodynamics; Aerospace engineering; Motion control; Orbital robotics; Payloads; Robots; Satellites; Space missions; Space technology; Tensile stress;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Intelligent Robots and Systems '93, IROS '93. Proceedings of the 1993 IEEE/RSJ International Conference on
Conference_Location :
Yokohama
Print_ISBN :
0-7803-0823-9
Type :
conf
DOI :
10.1109/IROS.1993.583915
Filename :
583915
Link To Document :
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