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] | ||
| 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 | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Advanced control of aircraft, rockets, and spacecraft / / Ashish Tewari
| Advanced control of aircraft, rockets, and spacecraft / / Ashish Tewari |
| Autore | Tewari Ashish |
| Edizione | [1st ed.] |
| 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 | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Advances in aerospace guidance, navigation and control : selected papers of the second CEAS Specialist Conference on Guidance, Navigation and Control / / Qiping Chu ... [et. al.], editors
| Advances in aerospace guidance, navigation and control : selected papers of the second CEAS Specialist Conference on Guidance, Navigation and Control / / Qiping Chu ... [et. al.], editors |
| Edizione | [1st ed. 2013.] |
| Pubbl/distr/stampa | Berlin ; ; Heidelberg, : Springer-Verlag, 2013 |
| Descrizione fisica | 1 online resource (773 p.) |
| Disciplina | 629.453 |
| Altri autori (Persone) | ChuQiping |
| Soggetto topico |
Flight control
Airplanes - Control systems Engineering mathematics Engineering |
| ISBN | 3-642-38253-3 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
Guidance and Control. Linear Parameter Varying Control of an Agile Missile Model Based on the Induced L 2-norm Framework / Raziye Tekin, Harald Pfifer -- Improving the Performance of an Actuator Control Scheme during Saturation / Chang How Lo, Hyo-Sang Shin, Antonios Tsourdos, Seung-Hwan Kim -- Concurrent Learning Adaptive Model Predictive Control / Girish Chowdhary [and others] -- Model Reference Adaptive Control of Mildly Non-Linear Systems with Time Varying Input Delays - Part I / James P. Nelson, Mark J. Balas, Richard S. Erwin -- Model Reference Adaptive Control of Mildly Non-Linear Systems with Time Varying Input Delays - Part II / James P. Nelson, Mark J. Balas, Richard S. Erwin -- Flight Control Algorithms for a Vertical Launch Air Defense Missile / Raziye Tekin, Ozgur Atesoglu, Kemal Leblebicioglu -- LFT Model Generation via ℓ1-Regularized Least Squares / Harald Pfifer, Simon Hecker -- An Impulsive Input Approach to Short Time Convergent Control for Linear Systems / Martin Weiss, Yuri Shtessel -- Model Formulation of Pursuit Problem with Two Pursuers and One Evader / Sergey S. Kumkov, Stéphane Le Ménec, Valerii S. Patsko -- Nonlinear Output-Feedback H [infinity symbol] Control for Spacecraft Attitude Control / Alon Capua [and others].
Estimation and Navigation. Rotorcraft System Identification: An Integrated Time-Frequency Domain Approach / Marco Bergamasco, Marco Lovera -- Air Data Sensor Fault Detection Using Kinematic Relations / Laurens van Eykeren, Qiping Chu -- A Multiple-Observer Scheme for Fault Detection, Isolation and Recovery of Satellite Thrusters / Antoine Abauzit, Julien Marzat -- A Spherical Coordinate Parametrization for an In-Orbit Bearings-Only Navigation Filter / Jonathan Grzymisch [and others] -- A New Substitution Based Recursive B-Splines Method for Aerodynamic Model Identification / Liguo Sun, Coen de Visser, Qiping Chu -- Spacecraft Fault Detection and Isolation System Design Using Decentralized Analytical Redundancy / Saurabh Indra, Louise Travé-Massuyès -- Flight Test Oriented Autopilot Design for Improved Aerodynamic Parameter Identification / Matthias Krings, Karsten Henning, Frank Thielecke -- A Flight State Estimator that Combines Stereo-Vision, INS, and Satellite Pseudo-Ranges / Franz Andert [and others] -- L1 Adaptive Control for Systems with Matched Stochastic Disturbance / Toufik Souanef, Federico Pinchetti, Walter Fichter. Atmospheric Applications. Decoupling the Eye: A Key toward a Robust Hovering for Sighted Aerial Robots / Augustin Manecy [and others] -- Flight Guidance and Control of a Tethered Glider in an Airborne Wind Energy Application / Sören Sieberling -- Lateral Fly by Wire Control System Dedicated to Future Small Aircraft / Matthias Heller, Thaddäus Baier, Falko Schuck -- Dynamic Trajectory Control of Gliders / Rui Dilão, João Fonseca -- Cooperative Autonomous Collision Avoidance System for Unmanned Aerial Vehicle / Yazdi Ibrahim Jenie, Erik-Jan van Kampen, Bart Remes -- Nonlinear Non-cascaded Reference Model Architecture for Flight Control Design / Fubiao Zhang, Florian Holzapfel, Matthias Heller -- Aircraft Longitudinal Guidance Based on a Spatial Reference / Hakim Bouadi, Daniel Choukroun, Felix Mora-Camino -- Adaptive Trajectory Controller for Generic Fixed-Wing Unmanned Aircraft / Maximilian Mühlegg [and others] -- Stereo Vision Based Obstacle Avoidance on Flapping Wing MAVs / Sjoerd Tijmons [and others] -- The Total Energy Control Concept for a Motor Glider / Maxim Lamp, Robert Luckner -- TECS Generalized Airplane Control System Design-An Update / Antonius A. Lambregts -- Integrated Modelling of an Unmanned High-Altitude Solar-Powered Aircraft for Control Law Design Analysis / Andreas Klöckner [and others] -- Design and Flight Testing of Nonlinear Autoflight Control Laws Incorporating Direct Lift Control / Thomas Lombaerts, Gertjan Looye -- A Frequency-Limited H2 Model Approximation Method with Application to a Medium-Scale Flexible Aircraft / Pierre Vuillemin, Charles Poussot-Vassal, Daniel Alazard -- Hardware-in-the-Loop Flight Simulator-An Essential Part in the Development Process for the Automatic Flight Control System of a Utility Aircraft / André Kaden, Bernd Boche, Robert Luckner -- Autonomous Wind Tunnel Free-Flight of a Flapping Wing MAV / Christophe De Wagter [and others] -- Application of Frequency-Limited Adaptive Quadrocopter Control / Kirk Y.W. Scheper [and others] -- Aeroservoelastic Investigations of a High-Aspect-Ratio Motor Glider / Flávio J. Silvestre. Space Applications. Relative Optical Navigation for a Lunar Lander Mission / Mark J. Verweld -- Toward an Autonomous Lunar Landing Based on Low-Speed Optic Flow Sensors / Guillaume Sabiron [and others] -- Online Estimation of Mean Orbital Elements with Control Inputs / Weichao Zhong, Pini Gurfil -- Flight Nutation Validation of the COS-B and EQUATOR-S Spacecraft / Hans Kuiper, Edward Bongers -- Fault-Tolerant Spacecraft Magnetic Attitude Control / Aviran Sadon, Daniel Choukroun -- GNC Challenges and Navigation Solutions for Active Debris Removal Mission / Erwan Kervendal, Thomas Chabot, Keyvan Kanani. |
| Record Nr. | UNINA-9910438051703321 |
| Berlin ; ; Heidelberg, : Springer-Verlag, 2013 | ||
| Lo trovi qui: Univ. Federico II | ||
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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] | ||
| 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] | ||
| 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->
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||
| Chichester, West Sussex, : John Wiley & Sons, Inc., 2013 | ||
| 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->
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||
| Chichester, West Sussex, : John Wiley & Sons, Inc., 2013 | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Aircraft flight dynamics and control / / Wayne Durham
| Aircraft flight dynamics and control / / 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-9910962792103321 |
Durham Wayne <1941->
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| Chichester, West Sussex, : John Wiley & Sons, Inc., 2013 | ||
| Lo trovi qui: Univ. Federico II | ||
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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 | ||
| Lo trovi qui: Univ. Federico II | ||
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