A Collection of Technical Papers: AIAA Aircraft Systems and Technology Meeting, August 20-22, 1979, New York, New YorkAmerican Institute of Aeronautics and Astronautics, 1979 - Aeronautics |
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... tion is not available to the BCS , the attitude command mode uses a direction cosine mechanization to compute vehicle attitudes through integrations of angular rates . A heading hold function becomes active when the BCS is not in a turn ...
... tion is not available to the BCS , the attitude command mode uses a direction cosine mechanization to compute vehicle attitudes through integrations of angular rates . A heading hold function becomes active when the BCS is not in a turn ...
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... tion ( laser trimming , chemical milling , or machin- ing ) removes excess material , leaving an efficient structural element with material buildups located in the section's flanges . This procedure greatly reduces tooling cost and ...
... tion ( laser trimming , chemical milling , or machin- ing ) removes excess material , leaving an efficient structural element with material buildups located in the section's flanges . This procedure greatly reduces tooling cost and ...
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... tion System ( DDARS ) has been implemented for use in flight testing of general avia- tion aircraft . The DDARS package , assemb- led from off - the - shelf components selected for use in aircraft where minimum weight and low power ...
... tion System ( DDARS ) has been implemented for use in flight testing of general avia- tion aircraft . The DDARS package , assemb- led from off - the - shelf components selected for use in aircraft where minimum weight and low power ...
Common terms and phrases
aerodynamic AIAA AIAA AIRCRAFT SYSTEMS aileron airfoil airplane altitude analysis angle of attack axisymmetric baseline bleed blowing CADAM canard capability centerbody characteristics chord components concept configuration cost cruise deflection delta wing drag dutch roll effects engine fighter flap flight test force fuel fuselage geometry ground high lift HiMAT improved increased increments induced drag inlet integrated leading edge leading-edge lift coefficient load Mach number maximum measured missile NACA nacelle NASA nozzle operation panel parameters payload performance pilot pitching pitching moment predicted pressure propulsion radar recovery reduced Reynolds number roll shown in Figure spanwise speed spin spoiler stability stall static strake structural subsonic supersonic surface tail takeoff techniques thrust vectoring tion trailing edge trim V/STOL vehicle velocity vertical vortex lift weight wind tunnel winglet