PPT-Flight Controls and Stability

Airplane Flight XPlane in the Classroom Stability Control Pitch nose moves up and down Control Pitch nose moves up and down Yaw nose moves left and right Stability Control Pitch nose moves up and down. 1 nt oductio 112 em O ie 113 Desi n Philos 114 em hi ectu Flight Deck Controls System Electronics ARINC 629 Data Bus Interface to Other Airplane Systems Electrical Power 115 nt ol urfa e tuation FlybyWire Actuation Mechanical Control 116 ault ol What . is the purpose of flight controls? . Describe what is a hydro-mechanical flight control system.. What . are the control surfaces of a primary flight control system?. What . is the purpose of the secondary flight control systems?. Define Static stability.. Define Dynamic stability.. Stability in an aircraft affects . what . two . aspects of an aircraft.. Define Lateral stability.. Describe the effect of wing dihedral.. Warm-Up – . Flight. Stability for. Straight and Level . Flight. Glider in Flight. Gliders Are Long . Distance Fliers. Gaining Altitude. Glider do not have an engine. Use rising air to gain altitude . Balsa Glider Flight. Jonathan L. Vigh and . Hugh E. Willoughby and Frank D. Marks and Mark . DeMaria. and Wayne . H. . Schubert. Colorado State . University, Florida International University, AOML Hurricane Research Division, NOAA-RAMMB, CSU. Forces Acting on an Aircraft. © 2015 Coast Flight Training. All Rights Reserved.. Thrust. Drag. Lift. Weight (or Load). Thrust. © 2015 Coast Flight Training. All Rights Reserved.. Moves the airplane through the air. Theoretical . and Practical . Challenges. Haithem. E . Taha. Mechanical and Aerospace Engineering. University . of California, Irvine. Cairo University . Aerospace Engineering Department . Tue, Mar 17, 2015. THE OBJECTIVE. To understand how the various aerodynamic forces act on an airplane and to know how to control those forces for safe flight. WHERE TO START?. Gather up your resource texts, the PTS and the FAA reference books and AC’s. Jenni. Tran. PRIMARY CONTROLS:. SECONDARY CONTROLS:. Analysis . and Design of Flapping-Wing MAVs. Haithem Taha. Mechanical and Aerospace Engineering. University . of California, Irvine. Vehicle Technology Directorate. Army Research Laboratory. Sep 10, 2015. Forces of Flight and Stability © 2011 Project Lead The Way, Inc. Aerospace Engineering Thrust Lift Drag Weight Forces on an Aircraft Four forces on an aircraft in flight: Weight: G ravitational attraction of the Earth Professional Yoke and Throttle Quadrant Simulation ControllerManche volant et quadrant de commande des gaz pour simulation de31vol proUSER GUIDEGUIDE DE L146UTILISATEURlogitechGcom34ENGLISH16FRANAIS2 Suitable for use in undergraduate aeronautical engineering curricula, this title is written for those first encountering the topic by clearly explaining the concepts and derivations of equations involved in aircraft flight mechanics. It also features insights about the A-10 based upon the author\'s career experience with this aircraft. Since the dawn of heavier-than-air flight and the discovery of the three axis flight control network, airplanes continue to employ the three primary controls: elevator, aileron, and rudder. . It should be noted that the same control inputs used by the pilot to fly small airplanes are used to control large aircraft..