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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
  • Miniature BLDC Motors for Flight Control Systems
    Though small in size, brushless DC mini motors serve a variety of critical roles in today's commercial and military aircraft. From delivering active force feedback to the pilot, thus reducing pilot workload and strain, to providing key inputs on controls inside the cockpit, motion solutions deliver
  • 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
  • Drone Development on Autopilot: How are Optical Components Used in Drones?
    Last month, NASA made a huge announcement - the success of its Ingenuity helicopter taking flight on Mars, making the UAV the first-ever aircraft to "make a powered, controlled flight on another planet1". To celebrate NASA's victory, Knight Optical - the leading supplier of premium-quality

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