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Advanced control of aircraft, rockets, and spacecraft [[electronic resource] /] / Ashish Tewari
| Advanced control of aircraft, rockets, and spacecraft [[electronic resource] /] / Ashish Tewari |
| Autore | Tewari Ashish |
| Pubbl/distr/stampa | Hoboken, N.J., : Wiley, 2011 |
| Descrizione fisica | 1 online resource (456 p.) |
| Disciplina |
500
629.11 |
| Collana | Aerospace Series |
| Soggetto topico |
Flight control
Airplanes - Control systems Space vehicles - Control systems Rockets (Aeronautics) - Control systems |
| ISBN |
1-119-97274-4
1-283-17775-7 9786613177759 1-119-97119-5 1-119-97120-9 |
| Classificazione | TEC002000 |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
Advanced Control of Aircraft, Spacecraft and Rockets; Contents; Series Preface; Preface; 1 Introduction; 1.1 Notation and Basic Definitions; 1.2 Control Systems; 1.2.1 Linear Tracking Systems; 1.2.2 Linear Time-Invariant Tracking Systems; 1.3 Guidance and Control of Flight Vehicles; 1.4 Special Tracking Laws; 1.4.1 Proportional Navigation Guidance; 1.4.2 Cross-Product Steering; 1.4.3 Proportional-Integral-Derivative Control; 1.5 Digital Tracking System; 1.6 Summary; Exercises; References; 2 Optimal Control Techniques; 2.1 Introduction; 2.2 Multi-variable Optimization
2.3 Constrained Minimization2.3.1 Equality Constraints; 2.3.2 Inequality Constraints; 2.4 Optimal Control of Dynamic Systems; 2.4.1 Optimality Conditions; 2.5 The Hamiltonian and the Minimum Principle; 2.5.1 Hamilton-Jacobi-Bellman Equation; 2.5.2 Linear Time-Varying System with Quadratic Performance Index; 2.6 Optimal Control with End-Point State Equality Constraints; 2.6.1 Euler-Lagrange Equations; 2.6.2 Special Cases; 2.7 Numerical Solution of Two-Point Boundary Value Problems; 2.7.1 Shooting Method; 2.7.2 Collocation Method; 2.8 Optimal Terminal Control with Interior Time Constraints 2.8.1 Optimal Singular Control2.9 Tracking Control; 2.9.1 Neighboring Extremal Method and Linear Quadratic Control; 2.10 Stochastic Processes; 2.10.1 Stationary Random Processes; 2.10.2 Filtering of Random Noise; 2.11 Kalman Filter; 2.12 Robust Linear Time-Invariant Control; 2.12.1 LQG/LTR Method; 2.12.2 H2/H8 Design Methods; 2.13 Summary; Exercises; References; 3 Optimal Navigation and Control of Aircraft; 3.1 Aircraft Navigation Plant; 3.1.1 Wind Speed and Direction; 3.1.2 Navigational Subsystems; 3.2 Optimal Aircraft Navigation; 3.2.1 Optimal Navigation Formulation 3.2.2 Extremal Solution of the Boundary-Value Problem: Long-Range Flight Example3.2.3 Great Circle Navigation; 3.3 Aircraft Attitude Dynamics; 3.3.1 Translational and Rotational Kinetics; 3.3.2 Attitude Relative to the Velocity Vector; 3.4 Aerodynamic Forces and Moments; 3.5 Longitudinal Dynamics; 3.5.1 Longitudinal Dynamics Plant; 3.6 Optimal Multi-variable Longitudinal Control; 3.7 Multi-input Optimal Longitudinal Control; 3.8 Optimal Airspeed Control; 3.8.1 LQG/LTR Design Example; 3.8.2 H8 Design Example; 3.8.3 Altitude and Mach Control; 3.9 Lateral-Directional Control Systems 3.9.1 Lateral-Directional Plant3.9.2 Optimal Roll Control; 3.9.3 Multi-variable Lateral-Directional Control: Heading-Hold Autopilot; 3.10 Optimal Control of Inertia-Coupled Aircraft Rotation; 3.11 Summary; Exercises; References; 4 Optimal Guidance of Rockets; 4.1 Introduction; 4.2 Optimal Terminal Guidance of Interceptors; 4.3 Non-planar Optimal Tracking System for Interceptors: 3DPN; 4.4 Flight in a Vertical Plane; 4.5 Optimal Terminal Guidance; 4.6 Vertical Launch of a Rocket (Goddard's Problem); 4.7 Gravity-Turn Trajectory of Launch Vehicles 4.7.1 Launch to Circular Orbit: Modulated Acceleration |
| Record Nr. | UNINA-9910139618703321 |
Tewari Ashish
|
||
| Hoboken, N.J., : Wiley, 2011 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Advanced control of aircraft, rockets, and spacecraft [[electronic resource] /] / Ashish Tewari
| Advanced control of aircraft, rockets, and spacecraft [[electronic resource] /] / Ashish Tewari |
| Autore | Tewari Ashish |
| Pubbl/distr/stampa | Hoboken, N.J., : Wiley, 2011 |
| Descrizione fisica | 1 online resource (456 p.) |
| Disciplina |
500
629.11 |
| Collana | Aerospace Series |
| Soggetto topico |
Flight control
Airplanes - Control systems Space vehicles - Control systems Rockets (Aeronautics) - Control systems |
| ISBN |
1-119-97274-4
1-283-17775-7 9786613177759 1-119-97119-5 1-119-97120-9 |
| Classificazione | TEC002000 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
Advanced Control of Aircraft, Spacecraft and Rockets; Contents; Series Preface; Preface; 1 Introduction; 1.1 Notation and Basic Definitions; 1.2 Control Systems; 1.2.1 Linear Tracking Systems; 1.2.2 Linear Time-Invariant Tracking Systems; 1.3 Guidance and Control of Flight Vehicles; 1.4 Special Tracking Laws; 1.4.1 Proportional Navigation Guidance; 1.4.2 Cross-Product Steering; 1.4.3 Proportional-Integral-Derivative Control; 1.5 Digital Tracking System; 1.6 Summary; Exercises; References; 2 Optimal Control Techniques; 2.1 Introduction; 2.2 Multi-variable Optimization
2.3 Constrained Minimization2.3.1 Equality Constraints; 2.3.2 Inequality Constraints; 2.4 Optimal Control of Dynamic Systems; 2.4.1 Optimality Conditions; 2.5 The Hamiltonian and the Minimum Principle; 2.5.1 Hamilton-Jacobi-Bellman Equation; 2.5.2 Linear Time-Varying System with Quadratic Performance Index; 2.6 Optimal Control with End-Point State Equality Constraints; 2.6.1 Euler-Lagrange Equations; 2.6.2 Special Cases; 2.7 Numerical Solution of Two-Point Boundary Value Problems; 2.7.1 Shooting Method; 2.7.2 Collocation Method; 2.8 Optimal Terminal Control with Interior Time Constraints 2.8.1 Optimal Singular Control2.9 Tracking Control; 2.9.1 Neighboring Extremal Method and Linear Quadratic Control; 2.10 Stochastic Processes; 2.10.1 Stationary Random Processes; 2.10.2 Filtering of Random Noise; 2.11 Kalman Filter; 2.12 Robust Linear Time-Invariant Control; 2.12.1 LQG/LTR Method; 2.12.2 H2/H8 Design Methods; 2.13 Summary; Exercises; References; 3 Optimal Navigation and Control of Aircraft; 3.1 Aircraft Navigation Plant; 3.1.1 Wind Speed and Direction; 3.1.2 Navigational Subsystems; 3.2 Optimal Aircraft Navigation; 3.2.1 Optimal Navigation Formulation 3.2.2 Extremal Solution of the Boundary-Value Problem: Long-Range Flight Example3.2.3 Great Circle Navigation; 3.3 Aircraft Attitude Dynamics; 3.3.1 Translational and Rotational Kinetics; 3.3.2 Attitude Relative to the Velocity Vector; 3.4 Aerodynamic Forces and Moments; 3.5 Longitudinal Dynamics; 3.5.1 Longitudinal Dynamics Plant; 3.6 Optimal Multi-variable Longitudinal Control; 3.7 Multi-input Optimal Longitudinal Control; 3.8 Optimal Airspeed Control; 3.8.1 LQG/LTR Design Example; 3.8.2 H8 Design Example; 3.8.3 Altitude and Mach Control; 3.9 Lateral-Directional Control Systems 3.9.1 Lateral-Directional Plant3.9.2 Optimal Roll Control; 3.9.3 Multi-variable Lateral-Directional Control: Heading-Hold Autopilot; 3.10 Optimal Control of Inertia-Coupled Aircraft Rotation; 3.11 Summary; Exercises; References; 4 Optimal Guidance of Rockets; 4.1 Introduction; 4.2 Optimal Terminal Guidance of Interceptors; 4.3 Non-planar Optimal Tracking System for Interceptors: 3DPN; 4.4 Flight in a Vertical Plane; 4.5 Optimal Terminal Guidance; 4.6 Vertical Launch of a Rocket (Goddard's Problem); 4.7 Gravity-Turn Trajectory of Launch Vehicles 4.7.1 Launch to Circular Orbit: Modulated Acceleration |
| Record Nr. | UNINA-9910818323903321 |
|
Tewari Ashish
|
||
| Hoboken, N.J., : Wiley, 2011 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Aircraft aerodynamic design : geometry and optimization / / András Sóbester, Alexander Forrester
| Aircraft aerodynamic design : geometry and optimization / / András Sóbester, Alexander Forrester |
| Autore | Sóbester András |
| Pubbl/distr/stampa | Chichester, England : , : Wiley, , 2015 |
| Descrizione fisica | 1 online resource (246 p.) |
| Disciplina | 629.134/1 |
| Collana |
Aerospace Series
THEi Wiley ebooks |
| Soggetto topico |
Airframes
Aerodynamics |
| ISBN |
1-5231-2340-0
1-118-53473-5 1-118-53474-3 1-118-53471-9 |
| Classificazione | TEC002000 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910132162503321 |
|
Sóbester András
|
||
| Chichester, England : , : Wiley, , 2015 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Aircraft aerodynamic design : geometry and optimization / / András Sóbester, Alexander Forrester
| Aircraft aerodynamic design : geometry and optimization / / András Sóbester, Alexander Forrester |
| Autore | Sóbester András |
| Pubbl/distr/stampa | Chichester, England : , : Wiley, , 2015 |
| Descrizione fisica | 1 online resource (246 p.) |
| Disciplina | 629.134/1 |
| Collana |
Aerospace Series
THEi Wiley ebooks |
| Soggetto topico |
Airframes
Aerodynamics |
| ISBN |
1-5231-2340-0
1-118-53473-5 1-118-53474-3 1-118-53471-9 |
| Classificazione | TEC002000 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910820810803321 |
|
Sóbester András
|
||
| Chichester, England : , : Wiley, , 2015 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Design and analysis of composite structures [[electronic resource] ] : with applications to aerospace structures / / Christos Kassapoglou
| Design and analysis of composite structures [[electronic resource] ] : with applications to aerospace structures / / Christos Kassapoglou |
| Autore | Kassapoglou Christos |
| Edizione | [2nd ed.] |
| Pubbl/distr/stampa | Chichester [England], : John Wiley & Sons Inc., 2013 |
| Descrizione fisica | 1 online resource (424 p.) |
| Disciplina |
629.134/31
629.13431 |
| Collana | Aerospace series |
| Soggetto topico |
Airframes - Materials
Composite construction Structural engineering |
| ISBN |
1-118-53693-2
1-118-53694-0 1-118-53695-9 |
| Classificazione | TEC002000 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
DESIGN AND ANALYSIS OF COMPOSITE STRUCTURES : WITH APPLICATIONS TO AEROSPACE STRUCTURES; Contents; About the Author; Series Preface; Preface to First Edition; Preface to Second Edition; 1 Applications of Advanced Composites in Aircraft Structures; References; 2 Cost of Composites: a Qualitative Discussion; 2.1 Recurring Cost; 2.2 Nonrecurring Cost; 2.3 Technology Selection; 2.4 Summary and Conclusions; Exercises; References; 3 Review of Classical Laminated Plate Theory; 3.1 Composite Materials: Definitions, Symbols and Terminology; 3.2 Constitutive Equations in Three Dimensions
3.2.1 Tensor Transformations3.3 Constitutive Equations in Two Dimensions: Plane Stress; Exercises; References; 4 Review of Laminate Strength and Failure Criteria; 4.1 Maximum Stress Failure Theory; 4.2 Maximum Strain Failure Theory; 4.3 Tsai-Hill Failure Theory; 4.4 Tsai-Wu Failure Theory; 4.5 Puck Failure Theory; 4.6 Other Failure Theories; References; 5 Composite Structural Components and Mathematical Formulation; 5.1 Overview of Composite Airframe; 5.1.1 The Structural Design Process: The Analyst's Perspective 5.1.2 Basic Design Concept and Process/Material Considerations for Aircraft Parts5.1.3 Sources of Uncertainty: Applied Loads, Usage and Material Scatter; 5.1.3.1 Knowledge of Applied Loads; 5.1.3.2 Variability in Usage; 5.1.3.3 Material Scatter; 5.1.4 Environmental Effects; 5.1.5 Effect of Damage; 5.1.6 Design Values and Allowables; 5.1.7 Additional Considerations of the Design Process; 5.2 Governing Equations; 5.2.1 Equilibrium Equations; 5.2.2 Stress-Strain Equations; 5.2.3 Strain-Displacement Equations; 5.2.4 von Karman Anisotropic Plate Equations for Large Deflections 5.3 Reductions of Governing Equations: Applications to Specific Problems5.3.1 Composite Plate under Localized In-Plane Load; 5.3.2 Composite Plate under Out-of-Plane Point Load; 5.4 Energy Methods; 5.4.1 Energy Expressions for Composite Plates; 5.4.1.1 Internal Strain Energy U; 5.4.1.2 External Work W; Exercises; References; 6 Buckling of Composite Plates; 6.1 Buckling of Rectangular Composite Plate under Biaxial Loading; 6.2 Buckling of Rectangular Composite Plate under Uniaxial Compression; 6.2.1 Uniaxial Compression, Three Sides Simply Supported, One Side Free 6.3 Buckling of Rectangular Composite Plate under Shear6.4 Buckling of Long Rectangular Composite Plates under Shear; 6.5 Buckling of Rectangular Composite Plates under Combined Loads; 6.6 Design Equations for Different Boundary Conditions and Load Combinations; Exercises; References; 7 Post-Buckling; 7.1 Post-Buckling Analysis of Composite Panels under Compression; 7.1.1 Application: Post-Buckled Panel under Compression; 7.2 Post-Buckling Analysis of Composite Plates under Shear; 7.2.1 Post-Buckling of Stiffened Composite Panels under Shear 7.2.1.1 Application: Post-Buckled Stiffened Fuselage Skin under Shear |
| Record Nr. | UNINA-9910141635403321 |
|
Kassapoglou Christos
|
||
| Chichester [England], : John Wiley & Sons Inc., 2013 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Design and analysis of composite structures [[electronic resource] ] : with applications to aerospace structures / / Christos Kassapoglou
| Design and analysis of composite structures [[electronic resource] ] : with applications to aerospace structures / / Christos Kassapoglou |
| Autore | Kassapoglou Christos |
| Edizione | [2nd ed.] |
| Pubbl/distr/stampa | Chichester [England], : John Wiley & Sons Inc., 2013 |
| Descrizione fisica | 1 online resource (424 p.) |
| Disciplina |
629.134/31
629.13431 |
| Collana | Aerospace series |
| Soggetto topico |
Airframes - Materials
Composite construction Structural engineering |
| ISBN |
1-118-53693-2
1-118-53694-0 1-118-53695-9 |
| Classificazione | TEC002000 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
DESIGN AND ANALYSIS OF COMPOSITE STRUCTURES : WITH APPLICATIONS TO AEROSPACE STRUCTURES; Contents; About the Author; Series Preface; Preface to First Edition; Preface to Second Edition; 1 Applications of Advanced Composites in Aircraft Structures; References; 2 Cost of Composites: a Qualitative Discussion; 2.1 Recurring Cost; 2.2 Nonrecurring Cost; 2.3 Technology Selection; 2.4 Summary and Conclusions; Exercises; References; 3 Review of Classical Laminated Plate Theory; 3.1 Composite Materials: Definitions, Symbols and Terminology; 3.2 Constitutive Equations in Three Dimensions
3.2.1 Tensor Transformations3.3 Constitutive Equations in Two Dimensions: Plane Stress; Exercises; References; 4 Review of Laminate Strength and Failure Criteria; 4.1 Maximum Stress Failure Theory; 4.2 Maximum Strain Failure Theory; 4.3 Tsai-Hill Failure Theory; 4.4 Tsai-Wu Failure Theory; 4.5 Puck Failure Theory; 4.6 Other Failure Theories; References; 5 Composite Structural Components and Mathematical Formulation; 5.1 Overview of Composite Airframe; 5.1.1 The Structural Design Process: The Analyst's Perspective 5.1.2 Basic Design Concept and Process/Material Considerations for Aircraft Parts5.1.3 Sources of Uncertainty: Applied Loads, Usage and Material Scatter; 5.1.3.1 Knowledge of Applied Loads; 5.1.3.2 Variability in Usage; 5.1.3.3 Material Scatter; 5.1.4 Environmental Effects; 5.1.5 Effect of Damage; 5.1.6 Design Values and Allowables; 5.1.7 Additional Considerations of the Design Process; 5.2 Governing Equations; 5.2.1 Equilibrium Equations; 5.2.2 Stress-Strain Equations; 5.2.3 Strain-Displacement Equations; 5.2.4 von Karman Anisotropic Plate Equations for Large Deflections 5.3 Reductions of Governing Equations: Applications to Specific Problems5.3.1 Composite Plate under Localized In-Plane Load; 5.3.2 Composite Plate under Out-of-Plane Point Load; 5.4 Energy Methods; 5.4.1 Energy Expressions for Composite Plates; 5.4.1.1 Internal Strain Energy U; 5.4.1.2 External Work W; Exercises; References; 6 Buckling of Composite Plates; 6.1 Buckling of Rectangular Composite Plate under Biaxial Loading; 6.2 Buckling of Rectangular Composite Plate under Uniaxial Compression; 6.2.1 Uniaxial Compression, Three Sides Simply Supported, One Side Free 6.3 Buckling of Rectangular Composite Plate under Shear6.4 Buckling of Long Rectangular Composite Plates under Shear; 6.5 Buckling of Rectangular Composite Plates under Combined Loads; 6.6 Design Equations for Different Boundary Conditions and Load Combinations; Exercises; References; 7 Post-Buckling; 7.1 Post-Buckling Analysis of Composite Panels under Compression; 7.1.1 Application: Post-Buckled Panel under Compression; 7.2 Post-Buckling Analysis of Composite Plates under Shear; 7.2.1 Post-Buckling of Stiffened Composite Panels under Shear 7.2.1.1 Application: Post-Buckled Stiffened Fuselage Skin under Shear |
| Record Nr. | UNINA-9910830263503321 |
|
Kassapoglou Christos
|
||
| Chichester [England], : John Wiley & Sons Inc., 2013 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Design and analysis of composite structures [[electronic resource] ] : with applications to aerospace structures / / Christos Kassapoglou
| Design and analysis of composite structures [[electronic resource] ] : with applications to aerospace structures / / Christos Kassapoglou |
| Autore | Kassapoglou Christos |
| Edizione | [2nd ed.] |
| Pubbl/distr/stampa | Chichester [England], : John Wiley & Sons Inc., 2013 |
| Descrizione fisica | 1 online resource (424 p.) |
| Disciplina |
629.134/31
629.13431 |
| Collana | Aerospace series |
| Soggetto topico |
Airframes - Materials
Composite construction Structural engineering |
| ISBN |
1-118-53693-2
1-118-53694-0 1-118-53695-9 |
| Classificazione | TEC002000 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
DESIGN AND ANALYSIS OF COMPOSITE STRUCTURES : WITH APPLICATIONS TO AEROSPACE STRUCTURES; Contents; About the Author; Series Preface; Preface to First Edition; Preface to Second Edition; 1 Applications of Advanced Composites in Aircraft Structures; References; 2 Cost of Composites: a Qualitative Discussion; 2.1 Recurring Cost; 2.2 Nonrecurring Cost; 2.3 Technology Selection; 2.4 Summary and Conclusions; Exercises; References; 3 Review of Classical Laminated Plate Theory; 3.1 Composite Materials: Definitions, Symbols and Terminology; 3.2 Constitutive Equations in Three Dimensions
3.2.1 Tensor Transformations3.3 Constitutive Equations in Two Dimensions: Plane Stress; Exercises; References; 4 Review of Laminate Strength and Failure Criteria; 4.1 Maximum Stress Failure Theory; 4.2 Maximum Strain Failure Theory; 4.3 Tsai-Hill Failure Theory; 4.4 Tsai-Wu Failure Theory; 4.5 Puck Failure Theory; 4.6 Other Failure Theories; References; 5 Composite Structural Components and Mathematical Formulation; 5.1 Overview of Composite Airframe; 5.1.1 The Structural Design Process: The Analyst's Perspective 5.1.2 Basic Design Concept and Process/Material Considerations for Aircraft Parts5.1.3 Sources of Uncertainty: Applied Loads, Usage and Material Scatter; 5.1.3.1 Knowledge of Applied Loads; 5.1.3.2 Variability in Usage; 5.1.3.3 Material Scatter; 5.1.4 Environmental Effects; 5.1.5 Effect of Damage; 5.1.6 Design Values and Allowables; 5.1.7 Additional Considerations of the Design Process; 5.2 Governing Equations; 5.2.1 Equilibrium Equations; 5.2.2 Stress-Strain Equations; 5.2.3 Strain-Displacement Equations; 5.2.4 von Karman Anisotropic Plate Equations for Large Deflections 5.3 Reductions of Governing Equations: Applications to Specific Problems5.3.1 Composite Plate under Localized In-Plane Load; 5.3.2 Composite Plate under Out-of-Plane Point Load; 5.4 Energy Methods; 5.4.1 Energy Expressions for Composite Plates; 5.4.1.1 Internal Strain Energy U; 5.4.1.2 External Work W; Exercises; References; 6 Buckling of Composite Plates; 6.1 Buckling of Rectangular Composite Plate under Biaxial Loading; 6.2 Buckling of Rectangular Composite Plate under Uniaxial Compression; 6.2.1 Uniaxial Compression, Three Sides Simply Supported, One Side Free 6.3 Buckling of Rectangular Composite Plate under Shear6.4 Buckling of Long Rectangular Composite Plates under Shear; 6.5 Buckling of Rectangular Composite Plates under Combined Loads; 6.6 Design Equations for Different Boundary Conditions and Load Combinations; Exercises; References; 7 Post-Buckling; 7.1 Post-Buckling Analysis of Composite Panels under Compression; 7.1.1 Application: Post-Buckled Panel under Compression; 7.2 Post-Buckling Analysis of Composite Plates under Shear; 7.2.1 Post-Buckling of Stiffened Composite Panels under Shear 7.2.1.1 Application: Post-Buckled Stiffened Fuselage Skin under Shear |
| Record Nr. | UNINA-9910840652303321 |
|
Kassapoglou Christos
|
||
| Chichester [England], : John Wiley & Sons Inc., 2013 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Sense and avoid in UAS [[electronic resource] ] : research and applications / / edited by Plamen Angelov
| Sense and avoid in UAS [[electronic resource] ] : research and applications / / edited by Plamen Angelov |
| Edizione | [2nd ed.] |
| Pubbl/distr/stampa | Hoboken, N.J., : Wiley, c2012 |
| Descrizione fisica | 1 online resource (381 p.) |
| Disciplina | 629.135/2 |
| Altri autori (Persone) | AngelovPlamen P |
| Collana | Aerospace series |
| Soggetto topico |
Airplanes - Collision avoidance
Drone aircraft - Control systems |
| ISBN |
1-280-58946-9
9786613619297 1-61344-917-8 1-119-96404-0 1-119-96395-8 |
| Classificazione | TEC002000 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto | pt. 1. Introduction -- pt. 2. Regulatory issues and human factors -- pt. 3. SAA methodologies -- pt. 4. SAA applications. |
| Record Nr. | UNINA-9910141291903321 |
| Hoboken, N.J., : Wiley, c2012 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Sense and avoid in UAS [[electronic resource] ] : research and applications / / edited by Plamen Angelov
| Sense and avoid in UAS [[electronic resource] ] : research and applications / / edited by Plamen Angelov |
| Edizione | [2nd ed.] |
| Pubbl/distr/stampa | Hoboken, N.J., : Wiley, c2012 |
| Descrizione fisica | 1 online resource (381 p.) |
| Disciplina | 629.135/2 |
| Altri autori (Persone) | AngelovPlamen P |
| Collana | Aerospace series |
| Soggetto topico |
Airplanes - Collision avoidance
Drone aircraft - Control systems |
| ISBN |
1-280-58946-9
9786613619297 1-61344-917-8 1-119-96404-0 1-119-96395-8 |
| Classificazione | TEC002000 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto | pt. 1. Introduction -- pt. 2. Regulatory issues and human factors -- pt. 3. SAA methodologies -- pt. 4. SAA applications. |
| Record Nr. | UNINA-9910815917203321 |
| Hoboken, N.J., : Wiley, c2012 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Spacecraft Systems Engineering [[electronic resource]]
| Spacecraft Systems Engineering [[electronic resource]] |
| Autore | Fortescue Peter |
| Edizione | [4th ed.] |
| Pubbl/distr/stampa | Chicester, : Wiley, 2011 |
| Descrizione fisica | 1 online resource (725 p.) |
| Disciplina |
629.47
629.474 |
| Altri autori (Persone) |
SwinerdGraham
StarkJohn |
| Soggetto topico |
Astronautics - Systems engineering
Astronautics -- Systems engineering Materials -- Congresses Space vehicles - Design and construction Space vehicles -- Design and construction Structural dynamics -- Congresses TECHNOLOGY & ENGINEERING / Aeronautics & Astronautics Mechanical Engineering Engineering & Applied Sciences Aeronautics Engineering & Astronautics |
| Soggetto genere / forma | Electronic books. |
| ISBN |
1-283-24036-X
9786613240361 1-118-30298-2 1-119-97100-4 1-119-97101-2 |
| Classificazione | TEC002000 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
SPACECRAFT SYSTEMS ENGINEERING; CONTENTS; List of Contributors; Preface to the Fourth Edition; Preface to the Third Edition; Preface to the Second Edition; Preface to the First Edition; List of Acronyms; 1 INTRODUCTION; 1.1 Payloads and Missions; 1.2 A System View of Spacecraft; 1.3 The Future; 2 THE SPACECRAFT ENVIRONMENT AND ITS EFFECT ON DESIGN; 2.1 Introduction; 2.2 Pre-Operational Spacecraft Environments; 2.3 Operational Spacecraft Environments; 2.4 Environmental Effects on Design; 3 DYNAMICS OF SPACECRAFT; 3.1 Introduction; 3.2 Trajectory Dynamics; 3.3 General Attitude Dynamics
3.4 Attitude Motion of Specific Types of Spacecraft3.5 Oscillatory Modes; 3.6 In Conclusion; Appendix: The Inertia Matrix; 4 CELESTIAL MECHANICS; 4.1 Introduction; 4.2 The Two-body Problem-Particle Dynamics; 4.3 Specifying the Orbit; 4.4 Orbit Perturbations; 4.5 Restricted Three-body Problem; 5 MISSION ANALYSIS; 5.1 Introduction; 5.2 Keplerian Orbit Transfers; 5.3 Mission Analysis; 5.4 Polar LEO/Remote-Sensing Satellites; 5.5 Satellite Constellations; 5.6 Geostationary Earth Orbits (GEO); 5.7 Highly Elliptic Orbits; 5.8 Interplanetary Missions; 6 PROPULSION SYSTEMS; 6.1 Systems Classification 6.2 Chemical Rockets6.3 Spacecraft Propulsion; 6.4 Electric Propulsion; 7 LAUNCH VEHICLES; 7.1 Introduction; 7.2 Basic Launch Vehicle Performance and Operation; 7.3 Spacecraft Launch Phases and Mission Planning; 7.4 The Ariane 5 Launch Vehicle; 7.5 US Crewed Launch Systems; 7.6 Small Launchers and Reusable Sub-Orbital Vehicles; 7.7 Re-Entry into Earth's Atmosphere; 7.8 Specific Launch Costs and Reliability; 8 SPACECRAFT STRUCTURES; 8.1 Introduction; 8.2 Design Requirements; 8.3 Material Selection; 8.4 Analysis; 8.5 Design Verification; 8.6 Impact Protection; 8.7 Configuration Examples 8.8 The Future of Space Structures9 ATTITUDE CONTROL; 9.1 Introduction; 9.2 ACS Overview; 9.3 The Spacecraft Attitude Response; 9.4 Torques and Torquers; 9.5 Attitude Measurement; 9.6 ACS Computation; 10 ELECTRICAL POWER SYSTEMS; 10.1 Introduction; 10.2 Power System Elements; 10.3 Primary Power Systems; 10.4 Secondary Power Systems: Batteries; 10.5 Power Management, Distribution and Control; 10.6 Power Budget; 11 THERMAL CONTROL OF SPACECRAFT; 11.1 Introduction; 11.2 The Thermal Environment; 11.3 Thermal Balance; 11.4 Thermal Analysis; 11.5 Thermal Design; 11.6 Thermal Technology 11.7 Thermal Design Verification11.8 Example of Satellite Thermal Design-XMM/Newton; 12 TELECOMMUNICATIONS; 12.1 Introduction; 12.2 Techniques of Radio Communications; 12.3 The Communications Payload; 12.4 Conclusion; 13 TELEMETRY, COMMAND, DATA HANDLING AND PROCESSING; 13.1 Introduction; 13.2 System Architecture; 13.3 Telemetry Data Formatting; 13.4 Telecommand; 13.5 Communication Techniques and Protocols; 13.6 On-Board Data Handling (OBDH) and Processing; 13.7 Technology; 13.8 Tools and Controlling Documents; 14 GROUND SEGMENT; 14.1 Introduction; 14.2 The Ground Station 14.3 Flight Dynamics |
| Record Nr. | UNINA-9910139607303321 |
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Fortescue Peter
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| Chicester, : Wiley, 2011 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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