Boeing Helicopters CH-47 Chinook by David A. Anderton

By David A. Anderton

Boeing Helicopters CH-47 Chinook

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Visconti, G. (2008): Airborne measurements and climatic change science: aircraft, balloons and UAV, Mem SAIt, vol. 79, pp. 849–852. 57. ; Hussein, I. ; Erwin, R. S. (2011): Risk-based sensor management for integrated detection and estimation, AIAA Journal of Guidance, Control and Dynamics, vol. 34, pp. 1767–1778. 58. ; Liu, J. (2012): Evaluation methods for the autonomy of unmanned systems, Chinese Science Bulletin, vol. 57, pp. 3409-3418. 59. ; Jump, M. (2014): Generating certification evidence for autonomous unmanned aircraft using model checking and simulation, AIAA Journal of Aerospace Information System, vol.

235–239. 22. Department of Defense (USA) (2013): Unmanned systems integrated roadmap: FY 2013–2038, ref. number 14–S–0553 (129 pages). 23. EASA (2013): Airworthiness certification of unmanned aircraft system (UAS), European aviation safety agency, report E. Y013–01. 24. Florio, F. (2006): Air Worthiness, Elsevier. 25. Francis, M. S. (2012): Unmanned air systems: challenge and opportunity, AIAA Journal of Aircraft, vol. 49, pp. 1652–1665. 26. Fregene, K. (2012): Unmanned aerial vehicles and control: Lockheed martin advanced technology laboratories, IEEE Control System Magazine, vol.

In the stability frame, aerodynamic coefficients can be calculated and aerodynamic forces (lift, drag and side forces) and aerodynamic moments (in pitch, roll and yaw) can be determined with respect to the body frame. The equations of motion for the rigid-body model have appeared in many textbooks [4, 82, 104]. 4). 114) where M are the applied moments such as the moment created by the gravity, the aerodynamic moments, the propulsion and control moments, the aerologic disturbances. 116) FB and TB are, respectively, the applied force and torque on the aircraft center of gravity.

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