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Uedu Open / Aircraft Stability and Control
16.333

Aircraft Stability and Control

Prof. Jonathan P. How | Fall 2004
Engineering Aerospace Engineering Aerodynamics Avionics Guidance and Control Systems
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CC BY-NC-SA 4.0
課程簡介
This class includes a brief review of applied aerodynamics and modern approaches in aircraft stability and control. Topics covered include static stability and trim; stability derivatives and characteristic longitudinal and lateral-directional motions; and physical effects of the wing, fuselage, and tail on aircraft motion. Control methods and systems are discussed, with emphasis on flight vehicle stabilization by classical and modern control techniques; time and frequency domain analysis of control system performance; and human-pilot models and pilot-in-the-loop controls with applications. Other topics covered include V/STOL stability, dynamics, and control during transition from hover to forward flight; parameter sensitivity; and handling quality analysis of aircraft through variable flight conditions. There will be a brief discussion of motion at high angles-of-attack, roll coupling, and other nonlinear flight regimes.
Course Information
SourceMIT 開放式課程
科系Aeronautics and Astronautics
LanguageEnglish
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