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Active flight controls [[electronic resource]]
| Active flight controls [[electronic resource]] |
| Pubbl/distr/stampa | [Washington, D.C.] : , : U.S. Dept. of Transportation, Federal Aviation Administration, , [1983] |
| Descrizione fisica | 8 pages : digital, PDF file |
| Collana | Advisory circular |
| Soggetto topico | Flight control |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910697894603321 |
| [Washington, D.C.] : , : U.S. Dept. of Transportation, Federal Aviation Administration, , [1983] | ||
| 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-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 | ||
| ||
Advances in flight control systems / / edited by Maria Agneta Balint
| Advances in flight control systems / / edited by Maria Agneta Balint |
| Pubbl/distr/stampa | Rijeka, Croatia : , : Intech, , [2011] |
| Descrizione fisica | 1 online resource (312 pages) : illustrations |
| Disciplina | 629.1326 |
| Soggetto topico | Flight control |
| ISBN | 953-51-6001-X |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910138269203321 |
| Rijeka, Croatia : , : Intech, , [2011] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Advances in guidance, navigation and control : proceedings of 2020 International Conference on Guidance, Navigation and Control, ICGNC 2020, Tianjin, China, October 23-25, 2020 / / Liang Yan, Haibin Duan, Xiang Yu, editors
| Advances in guidance, navigation and control : proceedings of 2020 International Conference on Guidance, Navigation and Control, ICGNC 2020, Tianjin, China, October 23-25, 2020 / / Liang Yan, Haibin Duan, Xiang Yu, editors |
| Pubbl/distr/stampa | Singapore : , : Springer, , [2022] |
| Descrizione fisica | 1 online resource (5416 pages) |
| Disciplina | 629.135 |
| Collana | Lecture notes in electrical engineering |
| Soggetto topico |
Guidance systems (Flight)
Flight control Aids to air navigation |
| ISBN |
981-15-8154-1
981-15-8155-X |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910743251803321 |
| Singapore : , : Springer, , [2022] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Aircraft flight dynamics and control [[electronic resource] /] / Wayne Durham
| Aircraft flight dynamics and control [[electronic resource] /] / Wayne Durham |
| Autore | Durham Wayne <1941-> |
| Pubbl/distr/stampa | Chichester, West Sussex, : John Wiley & Sons, Inc., 2013 |
| Descrizione fisica | 1 online resource (308 p.) |
| Disciplina | 629.132/3 |
| Collana | Aerospace series |
| Soggetto topico |
Aerodynamics
Flight Flight control Airplanes - Performance |
| Soggetto genere / forma | Electronic books. |
| ISBN |
1-118-64680-0
1-118-64679-7 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
Cover; Title Page; Copyright; Contents; Series Preface; Glossary; Chapter 1 Introduction; 1.1 Background; 1.2 Overview; 1.3 Customs and Conventions; References; Chapter 2 Coordinate Systems; 2.1 Background; 2.2 The Coordinate Systems; 2.2.1 The inertial reference frame, FI; 2.2.2 The earth-centered reference frame, FEC; 2.2.3 The earth-fixed reference frame, FE; 2.2.4 The local-horizontal reference frame, FH; 2.2.5 Body-fixed reference frames, FB; 2.2.6 Wind-axis system, FW; 2.2.7 Atmospheric reference frame; 2.3 Vector Notation; 2.4 Customs and Conventions; 2.4.1 Latitude and longitude
2.4.2 Body axes2.4.3 `The' body-axis system; 2.4.4 Aerodynamic angles; Problems; References; Chapter 3 Coordinate System Transformations; 3.1 Problem Statement; 3.2 Transformations; 3.2.1 Definitions; 3.2.2 Direction cosines; 3.2.3 Euler angles; 3.2.4 Euler parameters; 3.3 Transformations of Systems of Equations; 3.4 Customs and Conventions; 3.4.1 Names of Euler angles; 3.4.2 Principal values of Euler angles; Problems; Reference; Chapter 4 Rotating Coordinate Systems; 4.1 General; 4.2 Direction Cosines; 4.3 Euler Angles; 4.4 Euler Parameters; 4.5 Customs and Conventions 4.5.1 Angular velocity componentsProblems; Chapter 5 Inertial Accelerations; 5.1 General; 5.2 Inertial Acceleration of a Point; 5.2.1 Arbitrary moving reference frame; 5.2.2 Earth-centered moving reference frame; 5.2.3 Earth-fixed moving reference frame; 5.3 Inertial Acceleration of a Mass; 5.3.1 Linear acceleration; 5.3.2 Rotational acceleration; 5.4 States; 5.5 Customs and Conventions; 5.5.1 Linear velocity components; 5.5.2 Angular velocity components; 5.5.3 Forces; 5.5.4 Moments; 5.5.5 Groupings; Problems; Chapter 6 Forces and Moments; 6.1 General; 6.1.1 Assumptions; 6.1.2 State variables 6.1.3 State rates6.1.4 Flight controls; 6.1.5 Independent variables; 6.2 Non-Dimensionalization; 6.3 Non-Dimensional Coefficient Dependencies; 6.3.1 General; 6.3.2 Altitude dependencies; 6.3.3 Velocity dependencies; 6.3.4 Angle-of-attack dependencies; 6.3.5 Sideslip dependencies; 6.3.6 Angular velocity dependencies; 6.3.7 Control dependencies; 6.3.8 Summary of dependencies; 6.4 The Linear Assumption; 6.5 Tabular Data; 6.6 Customs and Conventions; Problems; Chapter 7 Equations of Motion; 7.1 General; 7.2 Body-Axis Equations; 7.2.1 Body-axis force equations; 7.2.2 Body-axis moment equations 7.2.3 Body-axis orientation equations (kinematic equations)7.2.4 Body-axis navigation equations; 7.3 Wind-Axis Equations; 7.3.1 Wind-axis force equations; 7.3.2 Wind-axis orientation equations (kinematic equations); 7.3.3 Wind-axis navigation equations; 7.4 Steady-State Solutions; 7.4.1 General; 7.4.2 Special cases; 7.4.3 The trim problem; Problems; Reference; Chapter 8 Linearization; 8.1 General; 8.2 Taylor Series; 8.3 Nonlinear Ordinary Differential Equations; 8.4 Systems of Equations; 8.5 Examples; 8.5.1 General; 8.5.2 A kinematic equation; 8.5.3 A moment equation; 8.5.4 A force equation 8.6 Customs and Conventions |
| Record Nr. | UNINA-9910463787503321 |
|
Durham Wayne <1941->
|
||
| Chichester, West Sussex, : John Wiley & Sons, Inc., 2013 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Aircraft flight dynamics and control [[electronic resource] /] / Wayne Durham
| Aircraft flight dynamics and control [[electronic resource] /] / Wayne Durham |
| Autore | Durham Wayne <1941-> |
| Pubbl/distr/stampa | Chichester, West Sussex, : John Wiley & Sons, Inc., 2013 |
| Descrizione fisica | xix, 286 p. : ill |
| Disciplina | 629.132/3 |
| Collana | Aerospace series |
| Soggetto topico |
Aerodynamics
Airplanes - Performance Flight control Flight |
| ISBN |
9781118646793
1118646797 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910796091203321 |
|
Durham Wayne <1941->
|
||
| Chichester, West Sussex, : John Wiley & Sons, Inc., 2013 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Aircraft flight dynamics and control [[electronic resource] /] / Wayne Durham
| Aircraft flight dynamics and control [[electronic resource] /] / Wayne Durham |
| Autore | Durham Wayne <1941-> |
| Edizione | [1st ed.] |
| Pubbl/distr/stampa | Chichester, West Sussex, : John Wiley & Sons, Inc., 2013 |
| Descrizione fisica | xix, 286 p. : ill |
| Disciplina | 629.132/3 |
| Collana | Aerospace series |
| Soggetto topico |
Aerodynamics
Airplanes - Performance Flight control Flight |
| ISBN |
9781118646793
1118646797 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
Cover -- Title Page -- Copyright -- Contents -- Series Preface -- Glossary -- Chapter 1 Introduction -- 1.1 Background -- 1.2 Overview -- 1.3 Customs and Conventions -- References -- Chapter 2 Coordinate Systems -- 2.1 Background -- 2.2 The Coordinate Systems -- 2.2.1 The inertial reference frame, FI -- 2.2.2 The earth-centered reference frame, FEC -- 2.2.3 The earth-fixed reference frame, FE -- 2.2.4 The local-horizontal reference frame, FH -- 2.2.5 Body-fixed reference frames, FB -- 2.2.6 Wind-axis system, FW -- 2.2.7 Atmospheric reference frame -- 2.3 Vector Notation -- 2.4 Customs and Conventions -- 2.4.1 Latitude and longitude -- 2.4.2 Body axes -- 2.4.3 `The' body-axis system -- 2.4.4 Aerodynamic angles -- Problems -- References -- Chapter 3 Coordinate System Transformations -- 3.1 Problem Statement -- 3.2 Transformations -- 3.2.1 Definitions -- 3.2.2 Direction cosines -- 3.2.3 Euler angles -- 3.2.4 Euler parameters -- 3.3 Transformations of Systems of Equations -- 3.4 Customs and Conventions -- 3.4.1 Names of Euler angles -- 3.4.2 Principal values of Euler angles -- Problems -- Reference -- Chapter 4 Rotating Coordinate Systems -- 4.1 General -- 4.2 Direction Cosines -- 4.3 Euler Angles -- 4.4 Euler Parameters -- 4.5 Customs and Conventions -- 4.5.1 Angular velocity components -- Problems -- Chapter 5 Inertial Accelerations -- 5.1 General -- 5.2 Inertial Acceleration of a Point -- 5.2.1 Arbitrary moving reference frame -- 5.2.2 Earth-centered moving reference frame -- 5.2.3 Earth-fixed moving reference frame -- 5.3 Inertial Acceleration of a Mass -- 5.3.1 Linear acceleration -- 5.3.2 Rotational acceleration -- 5.4 States -- 5.5 Customs and Conventions -- 5.5.1 Linear velocity components -- 5.5.2 Angular velocity components -- 5.5.3 Forces -- 5.5.4 Moments -- 5.5.5 Groupings -- Problems -- Chapter 6 Forces and Moments -- 6.1 General.
6.1.1 Assumptions -- 6.1.2 State variables -- 6.1.3 State rates -- 6.1.4 Flight controls -- 6.1.5 Independent variables -- 6.2 Non-Dimensionalization -- 6.3 Non-Dimensional Coefficient Dependencies -- 6.3.1 General -- 6.3.2 Altitude dependencies -- 6.3.3 Velocity dependencies -- 6.3.4 Angle-of-attack dependencies -- 6.3.5 Sideslip dependencies -- 6.3.6 Angular velocity dependencies -- 6.3.7 Control dependencies -- 6.3.8 Summary of dependencies -- 6.4 The Linear Assumption -- 6.5 Tabular Data -- 6.6 Customs and Conventions -- Problems -- Chapter 7 Equations of Motion -- 7.1 General -- 7.2 Body-Axis Equations -- 7.2.1 Body-axis force equations -- 7.2.2 Body-axis moment equations -- 7.2.3 Body-axis orientation equations (kinematic equations) -- 7.2.4 Body-axis navigation equations -- 7.3 Wind-Axis Equations -- 7.3.1 Wind-axis force equations -- 7.3.2 Wind-axis orientation equations (kinematic equations) -- 7.3.3 Wind-axis navigation equations -- 7.4 Steady-State Solutions -- 7.4.1 General -- 7.4.2 Special cases -- 7.4.3 The trim problem -- Problems -- Reference -- Chapter 8 Linearization -- 8.1 General -- 8.2 Taylor Series -- 8.3 Nonlinear Ordinary Differential Equations -- 8.4 Systems of Equations -- 8.5 Examples -- 8.5.1 General -- 8.5.2 A kinematic equation -- 8.5.3 A moment equation -- 8.5.4 A force equation -- 8.6 Customs and Conventions -- 8.6.1 Omission of -- 8.6.2 Dimensional derivatives -- 8.6.3 Added mass -- 8.7 The Linear Equations -- 8.7.1 Linear equations -- 8.7.2 Matrix forms of the linear equations -- Problems -- References -- Chapter 9 Solutions to the Linear Equations -- 9.1 Scalar Equations -- 9.2 Matrix Equations -- 9.3 Initial Condition Response -- 9.3.1 Modal analysis -- 9.4 Mode Sensitivity and Approximations -- 9.4.1 Mode sensitivity -- 9.4.2 Approximations -- 9.5 Forced Response -- 9.5.1 Transfer functions. 9.5.2 Steady-state response -- Problems -- Chapter 10 Aircraft Flight Dynamics -- 10.1 Example: Longitudinal Dynamics -- 10.1.1 System matrices -- 10.1.2 State transition matrix and eigenvalues -- 10.1.3 Eigenvector analysis -- 10.1.4 Longitudinal mode sensitivity and approximations -- 10.1.5 Forced response -- 10.2 Example: Lateral-Directional Dynamics -- 10.2.1 System matrices -- 10.2.2 State transition matrix and eigenvalues -- 10.2.3 Eigenvector analysis -- 10.2.4 Lateral-directional mode sensitivity and approximations -- 10.2.5 Forced response -- Problems -- References -- Chapter 11 Flying Qualities -- 11.1 General -- 11.1.1 Method -- 11.1.2 Specifications and standards -- 11.2 MIL-F-8785C Requirements -- 11.2.1 General -- 11.2.2 Longitudinal flying qualities -- 11.2.3 Lateral-directional flying qualitities -- Problems -- References -- Chapter 12 Automatic Flight Control -- 12.1 Simple Feedback Systems -- 12.1.1 First-order systems -- 12.1.2 Second-order systems -- 12.1.3 A general representation -- 12.2 Example Feedback Control Applications -- 12.2.1 Roll mode -- 12.2.2 Short-period mode -- 12.2.3 Phugoid -- 12.2.4 Coupled roll-spiral oscillation -- Problems -- References -- Chapter 13 Trends in Automatic Flight Control -- 13.1 Overview -- 13.2 Dynamic Inversion -- 13.2.1 The controlled equations -- 13.2.2 The kinematic equations -- 13.2.3 The complementary equations -- 13.3 Control Allocation -- 13.3.1 Background -- 13.3.2 Problem statement -- 13.3.3 Optimality -- 13.3.4 Sub-optimal solutions -- 13.3.5 Optimal solutions -- 13.3.6 Near-optimal solutions -- Problems -- References -- Appendix A Example Aircraft -- Reference -- Appendix B Linearization -- B.1 Derivation of Frequently Used Derivatives -- B.2 Non-dimensionalization of the Rolling Moment Equation -- B.3 Body Axis Z-Force and Thrust Derivatives. B.4 Non-dimensionalization of the Z-Force Equation -- Appendix C Derivation of Euler Parameters -- Appendix D Fedeeva's Algorithm -- Reference -- Appendix E MATLAB® Commands Used in the Text -- E.1 Using MATLAB® -- E.2 Eigenvalues and Eigenvectors -- E.3 State-Space Representation -- E.4 Transfer Function Representation -- E.5 Root Locus -- E.6 MATLAB® Functions (m-files) -- E.6.1 Example aircraft -- E.6.2 Mode sensitivity matrix -- E.6.3 Cut-and-try root locus gains -- E.7 Miscellaneous Applications and Notes -- E.7.1 Matrices -- E.7.2 Commands used to create Figures 10.2 and 10.3 -- Index. |
| Record Nr. | UNINA-9910814647003321 |
|
Durham Wayne <1941->
|
||
| Chichester, West Sussex, : John Wiley & Sons, Inc., 2013 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Aircraft flight test trajectory control / / P.K.A. Menon and R.A. Walker
| Aircraft flight test trajectory control / / P.K.A. Menon and R.A. Walker |
| Autore | Menon P. K. A (Padmanabhan K. A.) |
| Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Division, , 1988 |
| Descrizione fisica | 1 online resource (196 unnumbered pages) : illustrations |
| Altri autori (Persone) | WalkerR. A |
| Collana | NASA contractor report |
| Soggetto topico |
Automatic pilots
Control theory Controllers Flight control Flight paths Mathematical models |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910704923703321 |
|
Menon P. K. A (Padmanabhan K. A.)
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| Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Division, , 1988 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Analysis of aviation safety reporting system incident data associated with the technical challenges of the atmospheric environment safety technology project / / Colleen A. Withrow and Mary S. Reveley
| Analysis of aviation safety reporting system incident data associated with the technical challenges of the atmospheric environment safety technology project / / Colleen A. Withrow and Mary S. Reveley |
| Autore | Withrow Colleen A. |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , August 2014 |
| Descrizione fisica | 1 online resource (v, 46 pages) : color illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Aircraft safety
Airframes Flight control Ice formation Atmospheric composition |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910703642503321 |
|
Withrow Colleen A.
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , August 2014 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
