141,99 €
inkl. MwSt.
Versandkostenfrei*
Versandfertig in über 4 Wochen
Melden Sie sich für den Produktalarm an, um über die Verfügbarkeit des Produkts informiert zu werden.

  • Gebundenes Buch

"Flight Dynamics, first published in 2004, took 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…mehr

Produktbeschreibung
"Flight Dynamics, first published in 2004, took 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. The second edition will provide updates that cover new developments in aviation. Substantive changes include the addition of examples that relate to contemporary aircraft types, such as uninhabited air vehicles (UAVs), electrically powered airplanes, blended wing-body configurations, supersonic and hypersonic cruisers, and sub-orbital aerospace planes"--
Autorenporträt
Robert F. Stengel is professor emeritus of mechanical and aerospace engineering and former associate dean of engineering and applied science at Princeton University. The author of Optimal Control and Estimation, he has conducted flight research and taught graduate and undergraduate courses on aircraft flight dynamics and control for more than forty years. He was a principal designer of the Apollo Lunar Module's manual attitude control logic, and he contributed to the design of the Space Shuttle's guidance and control system.