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| Author | : Pierre T. Kabamba |
| Publisher | : Cambridge University Press |
| Total Pages | : 333 |
| Release | : 2014-08-29 |
| Genre | : Mathematics |
| ISBN | : 1107070945 |
This text covers fundamentals in navigation of modern aerospace vehicles. It is an excellent resource for both graduate students and practicing engineers.
| Author | : Don Pendleton |
| Publisher | : Gold Eagle |
| Total Pages | : 317 |
| Release | : 2011-12-01 |
| Genre | : Fiction |
| ISBN | : 1459282337 |
U.S. intelligence agencies are picking up chatter about something big coming their way. A series of calculated executions of undercover intelligence personnel in Washington, London and Pakistan convinces the Oval Office that this is the attack the world has feared. The Stony Man teams deploy to the hot spots, fighting to connect the dots in a plot to blow dirty bombs in Boston and Peshawar. And every minute counts as the warriors seek to smash a deadly alliance of terror that seems to have unlimited power and resources.
| Author | : Bong Wie |
| Publisher | : AIAA |
| Total Pages | : 692 |
| Release | : 1998 |
| Genre | : Mathematics |
| ISBN | : 9781563472619 |
A textbook that incorporates the latest methods used for the analysis of spacecraft orbital, attitude, and structural dynamics and control. Spacecraft dynamics is treated as a dynamic system with emphasis on practical applications, typical examples of which are the analysis and redesign of the pointing control system of the Hubble Space Telescope and the analysis of an active vibrations control for the COFS (Control of Flexible Structures) Mast Flight System. In addition to the three subjects mentioned above, dynamic systems modeling, analysis, and control are also discussed. Annotation copyrighted by Book News, Inc., Portland, OR
| Author | : N A Shneydor |
| Publisher | : Elsevier |
| Total Pages | : 276 |
| Release | : 1998-01-01 |
| Genre | : Technology & Engineering |
| ISBN | : 1782420592 |
The continuing evolving capability of guided weapons demands ever more knowledge of their development. This modern and comprehensive book covers the control aspect of guidance of missiles, torpedoes, robots, and even animal predators, from the viewpoint of the pursuer. The text studies trajectories, zones of interception, the required manoeuvre effort, time of flight, launch envelopes, and stability of the guidance process. Mathematics at first-year university level is the only prerequisite. Acquaintance with feedback control theory would be helpful to the reader. - Covers the control aspect of guidance of missiles, torpedoes, robots, and even animal predators, from the viewpoint of the pursuer - Studies trajectories, zones of interception, the required manoeuvre effort, time of flight, launch envelopes, and stability of the guidance process
| Author | : United States. Federal Aviation Administration |
| Publisher | : |
| Total Pages | : 68 |
| Release | : 1988 |
| Genre | : Airport terminals |
| ISBN | : |
| Author | : |
| Publisher | : Transportation Research Board |
| Total Pages | : 269 |
| Release | : 2011 |
| Genre | : Business & Economics |
| ISBN | : 0309213533 |
'TRB's Airport Cooperative Research Program (ACRP) Report 54: Resource Manual for Airport In-Terminal Concessions provides guidance on the development and implementation of airport concession programs. The report includes information on the airport concession process; concession goals; potential customers; developing a concession space plan and concession mix; the Airport Concessions Disadvantaged Business Enterprise (ACDBE) program; and concession procurement, contracting, and management practices"--Publisher's description.
| Author | : Jean Albert Kéchichian |
| Publisher | : Springer Nature |
| Total Pages | : 417 |
| Release | : 2021-04-12 |
| Genre | : Technology & Engineering |
| ISBN | : 3030646572 |
This book provides a comprehensive analysis of time-fixed terminal rendezvous around the Earth using chemical propulsion. The book has two main objectives. The first is to derive the mathematics of relative motion in near-circular orbit when subjected to perturbations emanating from the oblateness of the Earth, third-body gravity, and atmospheric drag. The mathematics are suitable for quick trajectory prediction and the creation of computer codes and efficient software to solve impulsive maneuvers and fly rendezvous missions. The second objective of this book is to show how the relative motion theory is applied to the exact precision-integrated, long-duration, time-fixed terminal rendezvous problem around the oblate Earth for the general elliptic orbit case. The contents are both theoretical and applied, with long-lasting value for aerospace engineers, trajectory designers, professors of orbital mechanics, and students at the graduate level and above.
| Author | : Shaoming He |
| Publisher | : Springer Nature |
| Total Pages | : 221 |
| Release | : 2020-05-13 |
| Genre | : Technology & Engineering |
| ISBN | : 3030473481 |
This book presents a comprehensive overview of the recent advances in the domain of optimal guidance, exploring the characteristics of various optimal guidance algorithms and their pros and cons. Optimal guidance is based on the concept of trajectory optimization, which minimizes the meaningful performance index while satisfying certain terminal constraints, and by properly designing the cost function the guidance command can serve as a desired pattern for a variety of mission objectives. The book allows readers to gain a deeper understanding of how optimal guidance law can be utilized to achieve different mission objectives for missiles and UAVs, and also explores the physical meaning and working principle of different new optimal guidance laws. In practice, this information is important in ensuring confidence in the performance and reliability of the guidance law when implementing it in a real-world system, especially in aerospace engineering where reliability is the first priority.
