Author: United States. Navy Department. Bureau of Aeronautics
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 724
Book Description
Fundamentals of Design of Piloted Aircraft Flight Control Systems: Automatic flight control systems for piloted aircraft
Author: United States. Navy Department. Bureau of Aeronautics
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 724
Book Description
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 724
Book Description
Fundamentals of Design of Piloted Aircraft Flight Control Systems: Methods of analysis and synthesis of piloted aircraft flight control systems
Author: United States. Navy Department. Bureau of Aeronautics
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 376
Book Description
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 376
Book Description
Fundamentals of Design of Piloted Aircraft Flight Control Systems: sup. Flight controls; human dynamic response study
Author: United States. Navy Department. Bureau of Aeronautics
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 182
Book Description
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 182
Book Description
Fundamentals of Design of Piloted Aircraft Flight Control Systems
Author: United States. Navy Department. Bureau of Aeronautics
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 416
Book Description
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 416
Book Description
Fundamentals of Design of Piloted Aircraft Flight Control Systems
Automatic Flight Control Systems
Author: Mohammad Sadraey
Publisher: Morgan & Claypool Publishers
ISBN: 1681737299
Category : Technology & Engineering
Languages : en
Pages : 175
Book Description
This book provides readers with a design approach to the automatic flight control systems (AFCS). The AFCS is the primary on-board tool for long flight operations, and is the foundation for the airspace modernization initiatives. In this text, AFCS and autopilot are employed interchangeably. It presents fundamentals of AFCS/autopilot, including primary subsystems, dynamic modeling, AFCS categories/functions/modes, servos/actuators, measurement devices, requirements, functional block diagrams, design techniques, and control laws. The book consists of six chapters. The first two chapters cover the fundamentals of AFCS and closed-loop control systems in manned and unmanned aircraft. The last four chapters present features of Attitude control systems (Hold functions), Flight path control systems (Navigation functions), Stability augmentation systems, and Command augmentation systems, respectively.
Publisher: Morgan & Claypool Publishers
ISBN: 1681737299
Category : Technology & Engineering
Languages : en
Pages : 175
Book Description
This book provides readers with a design approach to the automatic flight control systems (AFCS). The AFCS is the primary on-board tool for long flight operations, and is the foundation for the airspace modernization initiatives. In this text, AFCS and autopilot are employed interchangeably. It presents fundamentals of AFCS/autopilot, including primary subsystems, dynamic modeling, AFCS categories/functions/modes, servos/actuators, measurement devices, requirements, functional block diagrams, design techniques, and control laws. The book consists of six chapters. The first two chapters cover the fundamentals of AFCS and closed-loop control systems in manned and unmanned aircraft. The last four chapters present features of Attitude control systems (Hold functions), Flight path control systems (Navigation functions), Stability augmentation systems, and Command augmentation systems, respectively.
Methods of Analysis and Synthesis of Piloted Aircraft Flight Control Systems.Vol. 1. Fundamentals of Design of Piloted Aircraft Flight Control Systems
Airplane Flight Dynamics and Automatic Flight Controls
Author: Jan Roskam
Publisher: DARcorporation
ISBN: 9781884885181
Category : Science
Languages : en
Pages : 430
Book Description
"In this part, exhaustive coverage is provided of the methods for analysis and synthesis of automatic flight control systems using classical control theory. This widely used book has been updated with the latest software methods. Throughout this text, the practical (design) applications of the theory are stressed with many examples and illustrations. Aircraft stability and control characteristics are all heavily regulated by civil as well as by military airworthiness authorities for safety reasons. The role of the these safety regulations in the application of the theory is therefore stressed throughout. Airplane Flight Dynamics & Automatic Flight Controls, Part II, is an essential reference for all aeronautical engineers working in the area of stability and control, regardless of experience levels. The book minimizes reader confusion through a systematic progression of fundamentals: - Elastic airplane stability and control coefficients and derivatives - Method for determining the equilibrium and manufacturing shape of an elastic airplane - Subsonic and supersonic numerical examples of aeroelasticity effects on stability & control derivatives - Bode and root-locus plots with open and closed loop airplane applications, and coverage of inverse applications - Stability augmentation systems: pitch dampers, yaw dampers and roll dampers - Synthesis concepts of automatic flight control modes: control-stick steering, auto-pilot hold, speed control, navigation and automatic landing - Digital control systems using classical control theory applications with Z-transforms - Applications of classical control theory - Human pilot transfer functions." --DescripciĆ³n del editor.
Publisher: DARcorporation
ISBN: 9781884885181
Category : Science
Languages : en
Pages : 430
Book Description
"In this part, exhaustive coverage is provided of the methods for analysis and synthesis of automatic flight control systems using classical control theory. This widely used book has been updated with the latest software methods. Throughout this text, the practical (design) applications of the theory are stressed with many examples and illustrations. Aircraft stability and control characteristics are all heavily regulated by civil as well as by military airworthiness authorities for safety reasons. The role of the these safety regulations in the application of the theory is therefore stressed throughout. Airplane Flight Dynamics & Automatic Flight Controls, Part II, is an essential reference for all aeronautical engineers working in the area of stability and control, regardless of experience levels. The book minimizes reader confusion through a systematic progression of fundamentals: - Elastic airplane stability and control coefficients and derivatives - Method for determining the equilibrium and manufacturing shape of an elastic airplane - Subsonic and supersonic numerical examples of aeroelasticity effects on stability & control derivatives - Bode and root-locus plots with open and closed loop airplane applications, and coverage of inverse applications - Stability augmentation systems: pitch dampers, yaw dampers and roll dampers - Synthesis concepts of automatic flight control modes: control-stick steering, auto-pilot hold, speed control, navigation and automatic landing - Digital control systems using classical control theory applications with Z-transforms - Applications of classical control theory - Human pilot transfer functions." --DescripciĆ³n del editor.
Flight Control System Manuals: Automatic flight control systems for piloted aircraft
Author: Northrop Aircraft, Inc
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 382
Book Description
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 382
Book Description
Flight Control Systems
Author: Roger Pratt
Publisher: IET
ISBN: 9780852967669
Category : Technology & Engineering
Languages : en
Pages : 416
Book Description
Annotation Bridging the gap between academic research and real-world applications, this reference on modern flight control methods for fixed-wing aircraft deals with fundamentals of flight control systems design, then concentrates on applications based on the modern control methods used in the latest aircraft. The book is written for practicing engineers who are new to the aviation industry, postgraduate students in strategic or applied research, and advanced undergraduates. Some knowledge of classical control is assumed. Pratt is a member of IEEE and is UK Member for AIAA's Technical Committee on Guidance, Navigation and Control. Annotation c. Book News, Inc., Portland, OR (booknews.com)
Publisher: IET
ISBN: 9780852967669
Category : Technology & Engineering
Languages : en
Pages : 416
Book Description
Annotation Bridging the gap between academic research and real-world applications, this reference on modern flight control methods for fixed-wing aircraft deals with fundamentals of flight control systems design, then concentrates on applications based on the modern control methods used in the latest aircraft. The book is written for practicing engineers who are new to the aviation industry, postgraduate students in strategic or applied research, and advanced undergraduates. Some knowledge of classical control is assumed. Pratt is a member of IEEE and is UK Member for AIAA's Technical Committee on Guidance, Navigation and Control. Annotation c. Book News, Inc., Portland, OR (booknews.com)