MINIMUM-TIME FLIGHT PATHS OF SUPERSONIC AIRCRAFT (AIRCRAFT).

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Publisher :
ISBN 13 :
Total Pages : 352 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis MINIMUM-TIME FLIGHT PATHS OF SUPERSONIC AIRCRAFT (AIRCRAFT). by : DONGLONG SHEU

Download or read book MINIMUM-TIME FLIGHT PATHS OF SUPERSONIC AIRCRAFT (AIRCRAFT). written by DONGLONG SHEU and published by . This book was released on 1992 with total page 352 pages. Available in PDF, EPUB and Kindle. Book excerpt: three-dimensional formulations. The various problems differ in the final conditions imposed. From the analysis in each problem, the optimal aerodynamic and thrust controls are obtained and the piloting technique to achieve the minimum time is explained.

Three-dimensional, Minimum-time Flight Paths to a Point and Onto a Line for a Supersonic Aircraft with a Maximum Mach Number Constraint

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ISBN 13 :
Total Pages : 62 pages
Book Rating : 4.F/5 ( download)

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Book Synopsis Three-dimensional, Minimum-time Flight Paths to a Point and Onto a Line for a Supersonic Aircraft with a Maximum Mach Number Constraint by : Stanford University. Department of Aeronautics and Astronautics

Download or read book Three-dimensional, Minimum-time Flight Paths to a Point and Onto a Line for a Supersonic Aircraft with a Maximum Mach Number Constraint written by Stanford University. Department of Aeronautics and Astronautics and published by . This book was released on 1972 with total page 62 pages. Available in PDF, EPUB and Kindle. Book excerpt: Optimal control theory and the energy-state approximation are used to determine the thrust, altitude, and bank angle programs for minimum-time flight paths of a supersonic aircraft from an initial energy, heading, and horizontal position to a specified final energy, heading, and point or line in a horizontal plane. Constraints on maximum and minimum thrust, stall angle-of-attack, maximum Mach number, maximum dynamic pressure, and maximum normal load factor are considered. The problem is restricted to those cases in which the flight path is long enough that the maximum Mach number is reached during the flight. Numerical results are presented for a typical supersonic aircraft capable of Mach 2.0 flight. (Author).

Scientific and Technical Aerospace Reports

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Publisher :
ISBN 13 :
Total Pages : 1102 pages
Book Rating : 4.X/5 (4 download)

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Book Synopsis Scientific and Technical Aerospace Reports by :

Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1973 with total page 1102 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Optimal Trajectories in Atmospheric Flight

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Publisher : Elsevier
ISBN 13 : 0444601457
Total Pages : 421 pages
Book Rating : 4.4/5 (446 download)

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Book Synopsis Optimal Trajectories in Atmospheric Flight by : Nguyen Vinh

Download or read book Optimal Trajectories in Atmospheric Flight written by Nguyen Vinh and published by Elsevier. This book was released on 2012-12-02 with total page 421 pages. Available in PDF, EPUB and Kindle. Book excerpt: Optimal Trajectories in Atmospheric Flight deals with the optimization of trajectories in atmospheric flight. The book begins with a simple treatment of functional optimization followed by a discussion of switching theory. It then presents the derivation of the general equations of motion along with the basic knowledge in aerodynamics and propulsion necessary for the analysis of atmospheric flight trajectories. It goes on to the study of optimal trajectories by providing the general properties of the optimal aerodynamic controls and the integrals of motion. This is followed by discussions of high subsonic and supersonic flight, and approximation techniques to reduce the order of the problem for a fast computation of the optimal trajectory. The final chapters present analyses of optimal reentry trajectories and orbital maneuvers. This book is intended as a reference text for scientists and engineers wanting to get into the subject of optimal trajectories in atmospheric flight. If used for teaching purposes, the book is written in a self-contained way so that a selective use of the material is at the discretion of the lecturer. The first 11 chapters are sufficient for a one-semester course with emphasis on optimal maneuvers of high performance aircraft.

STAR

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Publisher :
ISBN 13 :
Total Pages : 936 pages
Book Rating : 4.:/5 (334 download)

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Book Synopsis STAR by :

Download or read book STAR written by and published by . This book was released on 1973 with total page 936 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Performance, Stability, Dynamics, and Control of Airplanes

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Publisher : AIAA
ISBN 13 : 9781600860997
Total Pages : 810 pages
Book Rating : 4.8/5 (69 download)

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Book Synopsis Performance, Stability, Dynamics, and Control of Airplanes by : Bandu N. Pamadi

Download or read book Performance, Stability, Dynamics, and Control of Airplanes written by Bandu N. Pamadi and published by AIAA. This book was released on 2004 with total page 810 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Flight Performance of Fixed and Rotary Wing Aircraft

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Publisher : Elsevier
ISBN 13 : 0080461034
Total Pages : 594 pages
Book Rating : 4.0/5 (84 download)

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Book Synopsis Flight Performance of Fixed and Rotary Wing Aircraft by : Antonio Filippone

Download or read book Flight Performance of Fixed and Rotary Wing Aircraft written by Antonio Filippone and published by Elsevier. This book was released on 2006-05-10 with total page 594 pages. Available in PDF, EPUB and Kindle. Book excerpt: Calculation and optimisation of flight performance is required to design or select new aircraft, efficiently operate existing aircraft, and upgrade aircraft. It provides critical data for aircraft certification, accident investigation, fleet management, flight regulations and safety. This book presents an unrivalled range of advanced flight performance models for both transport and military aircraft, including the unconventional ends of the envelopes. Topics covered include the numerical solution of supersonic acceleration, transient roll, optimal climb of propeller aircraft, propeller performance, long-range flight with en-route stop, fuel planning, zero-gravity flight in the atmosphere, VSTOL operations, ski jump from aircraft carrier, optimal flight paths at subsonic and supersonic speed, range-payload analysis of fixed- and rotary wing aircraft, performance of tandem helicopters, lower-bound noise estimation, sonic boom, and more.This book will be a valuable text for undergraduate and post-graduate level students of aerospace engineering. It will also be an essential reference and resource for practicing aircraft engineers, aircraft operations managers and organizations handling air traffic control, flight and flying regulations, standards, safety, environment, and the complex financial aspects of flying aircraft. - Unique coverage of fixed and rotary wing aircraft in a unified manner, including optimisation, emissions control and regulation. - Ideal for students, aeronautical engineering capstone projects, and for widespread professional reference in the aerospace industry. - Comprehensive coverage of computer-based solution of aerospace engineering problems; the critical analysis of performance data; and case studies from real world engineering experience. - Supported by end of chapter exercises

Take-off Distances of a Supersonic Transport Configuration as Affected by Airplane Rotation During the Take-off Run

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Publisher :
ISBN 13 :
Total Pages : 28 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Take-off Distances of a Supersonic Transport Configuration as Affected by Airplane Rotation During the Take-off Run by : Albert W. Hall

Download or read book Take-off Distances of a Supersonic Transport Configuration as Affected by Airplane Rotation During the Take-off Run written by Albert W. Hall and published by . This book was released on 1961 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt: An analytical study has been made to determine the effects of rotation speed, rotation angle, and rotation time on the take-off distance of a supersonic transport configuration. The takeoff distances were also determined at various rotation speeds to show the effects of such configuration changes as wing loading, maximum lift coefficient, thrust-weight ratio, and induced drag. (Author).

Government-wide Index to Federal Research & Development Reports

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Publisher :
ISBN 13 :
Total Pages : 1288 pages
Book Rating : 4.:/5 (2 download)

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Book Synopsis Government-wide Index to Federal Research & Development Reports by :

Download or read book Government-wide Index to Federal Research & Development Reports written by and published by . This book was released on 1966-12 with total page 1288 pages. Available in PDF, EPUB and Kindle. Book excerpt:

An Investigation of Aircraft Flight Paths for Minimum Time to Climb

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Publisher :
ISBN 13 :
Total Pages : 148 pages
Book Rating : 4.:/5 (287 download)

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Book Synopsis An Investigation of Aircraft Flight Paths for Minimum Time to Climb by : Philip Edwin Hong

Download or read book An Investigation of Aircraft Flight Paths for Minimum Time to Climb written by Philip Edwin Hong and published by . This book was released on 1965 with total page 148 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Minimum Fuel Horizontal Flightpaths in the Terminal Area

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Publisher :
ISBN 13 :
Total Pages : 42 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Minimum Fuel Horizontal Flightpaths in the Terminal Area by :

Download or read book Minimum Fuel Horizontal Flightpaths in the Terminal Area written by and published by . This book was released on 1981 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Energy: a Continuing Bibliography with Indexes

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Publisher :
ISBN 13 :
Total Pages : 452 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Energy: a Continuing Bibliography with Indexes by :

Download or read book Energy: a Continuing Bibliography with Indexes written by and published by . This book was released on 1974 with total page 452 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Advanced Aircraft Flight Performance

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Publisher : Cambridge University Press
ISBN 13 : 1107024005
Total Pages : 665 pages
Book Rating : 4.1/5 (7 download)

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Book Synopsis Advanced Aircraft Flight Performance by : Antonio Filippone

Download or read book Advanced Aircraft Flight Performance written by Antonio Filippone and published by Cambridge University Press. This book was released on 2012-12-17 with total page 665 pages. Available in PDF, EPUB and Kindle. Book excerpt: This unique book deals with the aeroplane at several levels and aims to simulate its flight performance using computer software.

Flight Dynamics

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Publisher : Princeton University Press
ISBN 13 : 1400866812
Total Pages : 864 pages
Book Rating : 4.4/5 (8 download)

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Book Synopsis Flight Dynamics by : Robert F. Stengel

Download or read book Flight Dynamics written by Robert F. Stengel and published by Princeton University Press. This book was released on 2015-01-27 with total page 864 pages. Available in PDF, EPUB and Kindle. Book excerpt: Flight Dynamics takes a new approach to the science and mathematics of aircraft flight, unifying principles of aeronautics with contemporary systems analysis. While presenting traditional material that is critical to understanding aircraft motions, it does so in the context of modern computational tools and multivariable methods. Robert Stengel devotes particular attention to models and techniques that are appropriate for analysis, simulation, evaluation of flying qualities, and control system design. He establishes bridges to classical analysis and results, and explores new territory that was treated only inferentially in earlier books. This book combines a highly accessible style of presentation with contents that will appeal to graduate students and to professionals already familiar with basic flight dynamics. Dynamic analysis has changed dramatically in recent decades, with the introduction of powerful personal computers and scientific programming languages. Analysis programs have become so pervasive that it can be assumed that all students and practicing engineers working on aircraft flight dynamics have access to them. Therefore, this book presents the principles, derivations, and equations of flight dynamics with frequent reference to MATLAB functions and examples. By using common notation and not assuming a strong background in aeronautics, Flight Dynamics will engage a wide variety of readers. Introductions to aerodynamics, propulsion, structures, flying qualities, flight control, and the atmospheric and gravitational environment accompany the development of the aircraft's dynamic equations.

Optimal Control with Aerospace Applications

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Publisher : Springer Science & Business Media
ISBN 13 : 1461489458
Total Pages : 286 pages
Book Rating : 4.4/5 (614 download)

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Book Synopsis Optimal Control with Aerospace Applications by : James M Longuski

Download or read book Optimal Control with Aerospace Applications written by James M Longuski and published by Springer Science & Business Media. This book was released on 2013-11-04 with total page 286 pages. Available in PDF, EPUB and Kindle. Book excerpt: Want to know not just what makes rockets go up but how to do it optimally? Optimal control theory has become such an important field in aerospace engineering that no graduate student or practicing engineer can afford to be without a working knowledge of it. This is the first book that begins from scratch to teach the reader the basic principles of the calculus of variations, develop the necessary conditions step-by-step, and introduce the elementary computational techniques of optimal control. This book, with problems and an online solution manual, provides the graduate-level reader with enough introductory knowledge so that he or she can not only read the literature and study the next level textbook but can also apply the theory to find optimal solutions in practice. No more is needed than the usual background of an undergraduate engineering, science, or mathematics program: namely calculus, differential equations, and numerical integration. Although finding optimal solutions for these problems is a complex process involving the calculus of variations, the authors carefully lay out step-by-step the most important theorems and concepts. Numerous examples are worked to demonstrate how to apply the theories to everything from classical problems (e.g., crossing a river in minimum time) to engineering problems (e.g., minimum-fuel launch of a satellite). Throughout the book use is made of the time-optimal launch of a satellite into orbit as an important case study with detailed analysis of two examples: launch from the Moon and launch from Earth. For launching into the field of optimal solutions, look no further!

Nonlinear Problems in Aviation and Aerospace

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Publisher : CRC Press
ISBN 13 : 9789056992224
Total Pages : 404 pages
Book Rating : 4.9/5 (922 download)

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Book Synopsis Nonlinear Problems in Aviation and Aerospace by : S. Sivasundaram

Download or read book Nonlinear Problems in Aviation and Aerospace written by S. Sivasundaram and published by CRC Press. This book was released on 2000-01-10 with total page 404 pages. Available in PDF, EPUB and Kindle. Book excerpt: The study of nonlinear phenomena in aviation and aerospace includes developments in computer technology and the use of nonlinear mathematical models. Nonlinearities are a feature of aircraft dynamics and flight control systems and need to respond to achieve stability and performance. This multiauthor volume comprises selected papers from the conference Nonlinear Problems in Aviation and Aerospace at Embry-Riddle Aeronautical University and additional invited papers from many distinguished scientists. Coverage includes orbit determination of a tethered satellite system using laser and radar tracking, and intelligent control of agile aircraft, flight control with and without control surfaces.

Technical Information Indexes

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Publisher :
ISBN 13 :
Total Pages : 148 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Technical Information Indexes by : United States. Naval Air Systems Command

Download or read book Technical Information Indexes written by United States. Naval Air Systems Command and published by . This book was released on 1975 with total page 148 pages. Available in PDF, EPUB and Kindle. Book excerpt: