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Results: 1-10 |
Results: 10
ADJUSTMENT PROCEDURE OF A HIGH-PRECISION DEPLOYABLE MESH ANTENNA FOR MUSES-B SPACECRAFT
Authors: TABATA M NATORI MC TASHIMA T INOUE T
Citation: M. Tabata et al., ADJUSTMENT PROCEDURE OF A HIGH-PRECISION DEPLOYABLE MESH ANTENNA FOR MUSES-B SPACECRAFT, Journal of intelligent material systems and structures, 8(9), 1997, pp. 801-809
AN OBJECT-ORIENTED MODELING APPROACH TO INTELLIGENT VARIABLE GEOMETRYTRUSSES
Authors: HUANG SY NATORI MC UMETANI Y NAKAI S KATUKURA H
Citation: Sy. Huang et al., AN OBJECT-ORIENTED MODELING APPROACH TO INTELLIGENT VARIABLE GEOMETRYTRUSSES, Journal of intelligent material systems and structures, 8(2), 1997, pp. 158-172
ACTIVE SHAPE CONTROL OF A DEPLOYABLE SPACE ANTENNA REFLECTOR
Authors: TABATA M NATORI MC
Citation: M. Tabata et Mc. Natori, ACTIVE SHAPE CONTROL OF A DEPLOYABLE SPACE ANTENNA REFLECTOR, Journal of intelligent material systems and structures, 7(2), 1996, pp. 235-240
MOTION CONTROL OF FREE-FLOATING VARIABLE GEOMETRY TRUSS .2. INVERSE KINEMATICS
Authors: HUANG SY NATORI MC MIURA K
Citation: Sy. Huang et al., MOTION CONTROL OF FREE-FLOATING VARIABLE GEOMETRY TRUSS .2. INVERSE KINEMATICS, Journal of guidance, control, and dynamics, 19(4), 1996, pp. 764-771
NUMERICAL-SOLUTION OF LARGE-DEFORMATION PROBLEMS INVOLVING STABILITY AND UNILATERAL CONSTRAINTS
Authors: SUN SM NATORI MC
Citation: Sm. Sun et Mc. Natori, NUMERICAL-SOLUTION OF LARGE-DEFORMATION PROBLEMS INVOLVING STABILITY AND UNILATERAL CONSTRAINTS, Computers & structures, 58(6), 1996, pp. 1245-1260
AN OBJECT-ORIENTED ARCHITECTURE FOR A FINITE-ELEMENT METHOD KNOWLEDGE-BASED SYSTEM
Authors: HUANG S NAKAI S KATUKURA H NATORI MC
Citation: S. Huang et al., AN OBJECT-ORIENTED ARCHITECTURE FOR A FINITE-ELEMENT METHOD KNOWLEDGE-BASED SYSTEM, International journal for numerical methods in engineering, 39(20), 1996, pp. 3497-3517
ADAPTIVITY DEMONSTRATION OF INFLATABLE RIGIDIZED INTEGRATED STRUCTURES (IRIS)
Authors: NATORI MC HIGUCHI K SEKINE K OKAZAKI K
Citation: Mc. Natori et al., ADAPTIVITY DEMONSTRATION OF INFLATABLE RIGIDIZED INTEGRATED STRUCTURES (IRIS), Acta astronautica, 37, 1995, pp. 59-67
PARAMETRIC QUADRATIC-PROGRAMMING METHOD FOR DYNAMIC CONTACT PROBLEMS WITH FRICTION
Authors: SUN SM TZOU HS NATORI MC
Citation: Sm. Sun et al., PARAMETRIC QUADRATIC-PROGRAMMING METHOD FOR DYNAMIC CONTACT PROBLEMS WITH FRICTION, AIAA journal, 32(2), 1994, pp. 371-378
ACTIVE ADHESION CONCEPTS FOR IN-ORBIT STRUCTURAL CONSTRUCTION
Authors: PARK KC NATORI MC
Citation: Kc. Park et Mc. Natori, ACTIVE ADHESION CONCEPTS FOR IN-ORBIT STRUCTURAL CONSTRUCTION, Journal of reinforced plastics and composites, 12(9), 1993, pp. 934-942
A COMPUTATIONAL-PROCEDURE FOR FLEXIBLE BEAMS WITH FRICTIONAL CONTACT CONSTRAINTS
Authors: SUN SM NATORI MC PARK KC
Citation: Sm. Sun et al., A COMPUTATIONAL-PROCEDURE FOR FLEXIBLE BEAMS WITH FRICTIONAL CONTACT CONSTRAINTS, International journal for numerical methods in engineering, 36(22), 1993, pp. 3781-3800
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