Arun Banerjee (American Institute of Aeronautics & US Astronautics
Flexible Multibody Dynamics
Efficient Formulations with Applications
Arun Banerjee (American Institute of Aeronautics & US Astronautics
Flexible Multibody Dynamics
Efficient Formulations with Applications
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This book demonstrates how to formulate the equations of mechanical systems. Providing methods of analysis of complex mechanical systems, the book has a clear focus on efficiency, equipping the reader with knowledge of algorithms that provide accurate results in reduced simulation time.
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This book demonstrates how to formulate the equations of mechanical systems. Providing methods of analysis of complex mechanical systems, the book has a clear focus on efficiency, equipping the reader with knowledge of algorithms that provide accurate results in reduced simulation time.
Hinweis: Dieser Artikel kann nur an eine deutsche Lieferadresse ausgeliefert werden.
Hinweis: Dieser Artikel kann nur an eine deutsche Lieferadresse ausgeliefert werden.
Produktdetails
- Produktdetails
- Verlag: Taylor & Francis Ltd
- 2 ed
- Seitenzahl: 408
- Erscheinungstermin: 26. August 2024
- Englisch
- Abmessung: 229mm x 152mm x 22mm
- Gewicht: 582g
- ISBN-13: 9781032139289
- ISBN-10: 1032139285
- Artikelnr.: 71236931
- Herstellerkennzeichnung
- Produktsicherheitsverantwortliche/r
- Europaallee 1
- 36244 Bad Hersfeld
- gpsr@libri.de
- Verlag: Taylor & Francis Ltd
- 2 ed
- Seitenzahl: 408
- Erscheinungstermin: 26. August 2024
- Englisch
- Abmessung: 229mm x 152mm x 22mm
- Gewicht: 582g
- ISBN-13: 9781032139289
- ISBN-10: 1032139285
- Artikelnr.: 71236931
- Herstellerkennzeichnung
- Produktsicherheitsverantwortliche/r
- Europaallee 1
- 36244 Bad Hersfeld
- gpsr@libri.de
Dr. Banerjee is a leading expert in flexible dynamics. After working in industry for Northrop Services, Martin Marietta Aerospace, Ford Aerospace, and Lockheed-Martin Advanced Technology Research Center, he developed DYNACON, Lockheed-Martin's multi-flexible-body dynamics and control simulation tool. He was awarded 1990 AIAA Engineer of the Year Award in Astronautics, was associate editor for the Journal of Guidance, Control, and Dynamics and is associate fellow of AIAA (American Institute of Aeronautics & Astronautics).
Introduction Background Material on Dynamics and Vibrations
Chapter 1 Derivation of Equations of Motion.
Chapter 2 Deployment, Station-Keeping, and Retrieval of a Flexible Tether
Connecting a Satellite to the Shuttle
Chapter 3 Kane's Method of Linearization Applied to the Dynamics of a Beam
in Large Overall Motion
Chapter 4 Dynamics of a Plate in Large Overall Motion
Chapter 5 Dynamics of an Arbitrary Flexible Body in Large Overall Motion
Chapter 6 Flexible Multibody Dynamics: Dense Matrix Formulation
Chapter 7 Component Mode Selection and Model Reduction: A Review
Chapter 8 Block-Diagonal Mass Matrix Formulation of Equations of Motion for
Flexible Multibody Systems
Chapter 9 Efficient Variables, Recursive Formulation, and Multi-Loop
Constraints in Flexible Multibody Dynamics
Chapter 10 An Order-n Formulation for Beams with Undergoing Large
Deflection and Large Base Motion. Chapter 11 Deployment/Retraction of Beams
and Cables from Moving Vehicles: Small Deflection Analysis, and Variable-N
Order-N Formulations for Large Deflection
Chapter 12 Flexible Rocket Dynamics, Using Geometric Softness and a
Block-Diagonal Mass Matrix
Chapter 13 Large Amplitude Fuel Slosh in Spacecraft in Large Overall Motion
Appendix A: Modal Integrals for an Arbitrary Flexible Body
Appendix B: Flexible Multibody Dynamics for Small Overall Motion
Appendix C: A FORTRAN Code of the Order-n Algorithm: Application to an
Example
Chapter 1 Derivation of Equations of Motion.
Chapter 2 Deployment, Station-Keeping, and Retrieval of a Flexible Tether
Connecting a Satellite to the Shuttle
Chapter 3 Kane's Method of Linearization Applied to the Dynamics of a Beam
in Large Overall Motion
Chapter 4 Dynamics of a Plate in Large Overall Motion
Chapter 5 Dynamics of an Arbitrary Flexible Body in Large Overall Motion
Chapter 6 Flexible Multibody Dynamics: Dense Matrix Formulation
Chapter 7 Component Mode Selection and Model Reduction: A Review
Chapter 8 Block-Diagonal Mass Matrix Formulation of Equations of Motion for
Flexible Multibody Systems
Chapter 9 Efficient Variables, Recursive Formulation, and Multi-Loop
Constraints in Flexible Multibody Dynamics
Chapter 10 An Order-n Formulation for Beams with Undergoing Large
Deflection and Large Base Motion. Chapter 11 Deployment/Retraction of Beams
and Cables from Moving Vehicles: Small Deflection Analysis, and Variable-N
Order-N Formulations for Large Deflection
Chapter 12 Flexible Rocket Dynamics, Using Geometric Softness and a
Block-Diagonal Mass Matrix
Chapter 13 Large Amplitude Fuel Slosh in Spacecraft in Large Overall Motion
Appendix A: Modal Integrals for an Arbitrary Flexible Body
Appendix B: Flexible Multibody Dynamics for Small Overall Motion
Appendix C: A FORTRAN Code of the Order-n Algorithm: Application to an
Example
Introduction Background Material on Dynamics and Vibrations
Chapter 1 Derivation of Equations of Motion.
Chapter 2 Deployment, Station-Keeping, and Retrieval of a Flexible Tether
Connecting a Satellite to the Shuttle
Chapter 3 Kane's Method of Linearization Applied to the Dynamics of a Beam
in Large Overall Motion
Chapter 4 Dynamics of a Plate in Large Overall Motion
Chapter 5 Dynamics of an Arbitrary Flexible Body in Large Overall Motion
Chapter 6 Flexible Multibody Dynamics: Dense Matrix Formulation
Chapter 7 Component Mode Selection and Model Reduction: A Review
Chapter 8 Block-Diagonal Mass Matrix Formulation of Equations of Motion for
Flexible Multibody Systems
Chapter 9 Efficient Variables, Recursive Formulation, and Multi-Loop
Constraints in Flexible Multibody Dynamics
Chapter 10 An Order-n Formulation for Beams with Undergoing Large
Deflection and Large Base Motion. Chapter 11 Deployment/Retraction of Beams
and Cables from Moving Vehicles: Small Deflection Analysis, and Variable-N
Order-N Formulations for Large Deflection
Chapter 12 Flexible Rocket Dynamics, Using Geometric Softness and a
Block-Diagonal Mass Matrix
Chapter 13 Large Amplitude Fuel Slosh in Spacecraft in Large Overall Motion
Appendix A: Modal Integrals for an Arbitrary Flexible Body
Appendix B: Flexible Multibody Dynamics for Small Overall Motion
Appendix C: A FORTRAN Code of the Order-n Algorithm: Application to an
Example
Chapter 1 Derivation of Equations of Motion.
Chapter 2 Deployment, Station-Keeping, and Retrieval of a Flexible Tether
Connecting a Satellite to the Shuttle
Chapter 3 Kane's Method of Linearization Applied to the Dynamics of a Beam
in Large Overall Motion
Chapter 4 Dynamics of a Plate in Large Overall Motion
Chapter 5 Dynamics of an Arbitrary Flexible Body in Large Overall Motion
Chapter 6 Flexible Multibody Dynamics: Dense Matrix Formulation
Chapter 7 Component Mode Selection and Model Reduction: A Review
Chapter 8 Block-Diagonal Mass Matrix Formulation of Equations of Motion for
Flexible Multibody Systems
Chapter 9 Efficient Variables, Recursive Formulation, and Multi-Loop
Constraints in Flexible Multibody Dynamics
Chapter 10 An Order-n Formulation for Beams with Undergoing Large
Deflection and Large Base Motion. Chapter 11 Deployment/Retraction of Beams
and Cables from Moving Vehicles: Small Deflection Analysis, and Variable-N
Order-N Formulations for Large Deflection
Chapter 12 Flexible Rocket Dynamics, Using Geometric Softness and a
Block-Diagonal Mass Matrix
Chapter 13 Large Amplitude Fuel Slosh in Spacecraft in Large Overall Motion
Appendix A: Modal Integrals for an Arbitrary Flexible Body
Appendix B: Flexible Multibody Dynamics for Small Overall Motion
Appendix C: A FORTRAN Code of the Order-n Algorithm: Application to an
Example