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Dynamics and Design of Space Nets for Orbital Capture [[electronic resource] /] / by Leping Yang, Qingbin Zhang, Ming Zhen, Haitao Liu
Dynamics and Design of Space Nets for Orbital Capture [[electronic resource] /] / by Leping Yang, Qingbin Zhang, Ming Zhen, Haitao Liu
Autore Yang Leping
Edizione [1st ed. 2017.]
Pubbl/distr/stampa Berlin, Heidelberg : , : Springer Berlin Heidelberg : , : Imprint : Springer, , 2017
Descrizione fisica 1 online resource (XV, 174 p. 148 illus.)
Disciplina 629.1
Soggetto topico Aerospace engineering
Astronautics
Vibration
Dynamical systems
Dynamics
System safety
Aerospace Technology and Astronautics
Vibration, Dynamical Systems, Control
Security Science and Technology
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Nota di contenuto Introduction -- Cable dynamics elements -- Dynamics of space nets -- Simulation of space net capture process -- Deployment dynamics of rotating space net -- Dynamics of tethered combination system -- Ground and airdrop test -- .
Record Nr. UNINA-9910254322303321
Yang Leping  
Berlin, Heidelberg : , : Springer Berlin Heidelberg : , : Imprint : Springer, , 2017
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
On-Orbit Operations Optimization [[electronic resource] ] : Modeling and Algorithms / / by Leping Yang, Yanwei Zhu, Xianhai Ren, Yuanwen Zhang
On-Orbit Operations Optimization [[electronic resource] ] : Modeling and Algorithms / / by Leping Yang, Yanwei Zhu, Xianhai Ren, Yuanwen Zhang
Autore Yang Leping
Edizione [1st ed. 2014.]
Pubbl/distr/stampa New York, NY : , : Springer New York : , : Imprint : Springer, , 2014
Descrizione fisica 1 online resource (130 p.)
Disciplina 629.4
Collana SpringerBriefs in Optimization
Soggetto topico Mathematical optimization
Aerospace engineering
Astronautics
Operations research
Management science
Mathematical models
Algorithms
Optimization
Aerospace Technology and Astronautics
Operations Research, Management Science
Mathematical Modeling and Industrial Mathematics
ISBN 1-4939-0838-3
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Nota di contenuto Preface; Acknowledgments; Contents; List of Abbreviations; Chapter 1: Introduction; 1.1 Background; 1.1.1 On-Orbit Servicing Concept; 1.1.2 Key Technology Areas; 1.2 On-Orbit Servicing Operations; 1.3 Optimization Problem; 1.3.1 Constraints; 1.3.2 Dynamics; 1.3.3 Algorithms; 1.4 Outline of the Book; References; Chapter 2: Spacecraft Multi-Mission Planning; 2.1 Problem Formulation; 2.1.1 Planning Model; 2.1.1.1 Decision Variables; 2.1.1.2 Cost Function; 2.1.1.3 Constraints; 2.1.2 Solution Strategy; 2.2 Integer Programming Method for Mission Assignment; 2.2.1 Planning Model; 2.2.2 Algorithms
2.2.3 Numerical Simulation2.3 HGABB for One-to-N Spacecraft Mission Planning; 2.3.1 Planning Model; 2.3.2 Algorithms; 2.3.3 Numerical Simulation; References; Chapter 3: Far-Range Orbital Maneuver Planning; 3.1 Problem Formulation; 3.1.1 Lambert Solution; 3.1.2 Multi-Impulse Trajectory Planning Model; 3.2 Genetic Algorithm for Multi-Impulse Planning; 3.2.1 Genetic Algorithm; 3.2.2 Planning Model; 3.2.3 Numerical Simulation; 3.3 Random Optimization for Multi-Impulse Planning; 3.3.1 Randomized A* Tree Expansion Algorithm; 3.3.2 Planning Model; 3.3.3 Numerical Simulation; References
Chapter 4: Proximity Relative Motion Planning4.1 Problem Formulation; 4.2 Sequential Quadratic Programming for Impulse Thrust Mode; 4.2.1 SQP Algorithm; 4.2.2 Two-Impulse Maneuver Model; 4.2.2.1 Near-Circular Reference Orbit; 4.2.2.2 Elliptical Reference Orbit; 4.2.3 Two-Impulse Trajectory Planning Model; 4.2.4 Numerical Simulation; 4.3 LP for Bang-Bang Thrust Mode; 4.3.1 LP Algorithm; 4.3.1.1 Inequality Constraint; 4.3.1.2 Nonconvex Constraint; 4.3.1.3 Free Decision Variable; 4.3.2 Discrete Dynamic Model; 4.3.3 Constraint Linearization; 4.3.3.1 State Constraint; 4.3.3.2 Control Constraint
4.3.3.3 Safety Constraint4.3.4 Planning Model; 4.3.5 Numerical Simulation; 4.4 Pontryagin ́s Maximum Principle for Constant Low Thrust Mode; 4.4.1 Pontryagin ́s Maximum Principle; 4.4.2 Dynamic Model; 4.4.3 Planning Model; 4.4.3.1 Minimum-Time Maneuver; 4.4.3.2 Minimum-Fuel Maneuver; 4.4.4 Numerical Simulation; 4.5 hp-APM for Local Inspection Trajectory Planning; 4.5.1 Mission Formulation; 4.5.2 6-DOF Coupled Dynamic Model; 4.5.3 Planning Model; 4.5.4 hp-APM; 4.5.5 Numerical Simulation; 4.6 IAPF for Close Proximity Inspection; 4.6.1 Mission Formulation; 4.6.2 IAPF Algorithm
4.6.3 Control Parameter Optimization4.6.4 Numerical Simulation; 4.7 IDVD for the Maneuvered Customer; 4.7.1 Mission Formulation; 4.7.2 IDVD Algorithm; 4.7.2.1 Translational Motion Planning; 4.7.2.2 Rotational Motion Planning; 4.7.3 Planning Model; 4.7.4 Numerical Simulation; References; Chapter 5: Multi-Spacecraft Coordinated Planning; 5.1 Problem Formulation; 5.1.1 Dynamic Models; 5.1.2 Mission Configurations; 5.1.3 Coordinated Planning; 5.2 Cyclic Pursuit Method; 5.2.1 Fundamentals; 5.2.2 Cyclic Pursuit Control Law; 5.2.2.1 Impulsive Thruster Control Law
5.2.2.2 Continuous Thruster Control Law
Record Nr. UNINA-9910299966803321
Yang Leping  
New York, NY : , : Springer New York : , : Imprint : Springer, , 2014
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui