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  • Aircraft and Rotorcraft System Identification: Engineering Methods with Flight-Test Examples
    Aircraft and Rotorcraft System Identification: Engineering Methods with Flight-Test Examples. Assuming knowledge of aeronautics, Laplace transforms, and flight dynamics and classical control, this text presents proven methods, practical guidelines, and real-world flight-test results for a wide
  • Introduction to Aircraft Flight Mechanics: Performance, Static Stability, Dynamic Stability, and Classical Feedback Control
    Introduction to Aircraft Flight Mechanics: Performance, Static Stability, Dynamic Stability, and Classical Feedback Control. Based on a successful 15-year approach to teaching aircraft flight mechanics at the U.S. Air Force Academy, this informative book clearly explains all the concepts
  • Flight Control Systems: Practical Issues in Design and Implementation
    Flight Control Systems: Practical Issues in Design and Implementation. Bridging the gap between academic research and real-world applications, this reference deals with fundamentals of flight control systems design, then concentrates on applications based on the modern control methods used
  • Software Enabled Control
    . in general, and autonomous aircraft in particular. Control, in this context,. should not be interpreted in some narrow sense. Here it encompasses algorithms. for inner-loop regulation as well as supervisory and mission-level. optimization, modeling and estimation of vehicle dynamics and environmental
  • Small-scale Turbo Compressors for More Efficient Take-off/Landing and Cruise of Future Aircraft
    and increasing efficiency due to CO2 emissions and global warming. Prof. Zha and his team from the University of Miami conduct research in the area of active flow control concepts for ultra-high lift coefficient, the so-called Super-Lift condition, by energizing the boundary layer of airfoils. This principle
  • Simulating Base-Shake Environmental Testing
    In most military aircraft and spacecraft applications, each. payload structure must be pre-tested on a shake table to ensure. that it can withstand the vibration environment that it. will experience during flight. Shaker testing is done using a. control PSD which is designed to realistically
  • Digital Cameras in Unmanned Aerial Vehicles (UAV) for Military and Commercial Uses
    An Unmanned Aerial Vehicle (UAV) is an aircraft that flies without a human pilot onboard, controlled remotely or flown autonomously via pre-programmed flight plans or other automated guidance systems. Traditionally, UAVs were largely deployed in military missions, but are increasingly being adopted
  • Taking to the High Skies with maxon motors
    At an altitude of 11 kilometers above the surface of the earth, the air is very thin. Modern pressure cabins and an environmental control system (ECS) ensure a pleasant atmosphere in commercial aircraft. In the new Boeing 787, also known as the Dreamliner, a special air-conditioning system further

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