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Systems design driven by sensors Pasadena
Detectors 1 Title
P1398 American Institute of Aeronautics and Astro
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AASIR aerodynamic aeroelastic AIAA Aileron aircraft airfoil altitude angle antenna aperture approach array azimuth bandwidth boundary layer calibration charge-coupled device configuration cooler cooling correlation cryogen cues detector Dev RMS display dynamic effects engine equations error experiment experimental Figure filter flight flight simulator flutter frequency G-seat gimbal heat Helmholtz resonance infrared input instruments launch linear load Mach number maneuvers measured ment missiles mission module motion NASA noise Nusselt operation optical orbit parameters payload performance pilot porosity pressure probe problems processing radar radiator range red/blue rod wall roll sampling scan sensor shown in Fig Shuttle signal simulator SIRTF space spacecraft Spacelab spectrum stability stratospheric surface synthetic aperture radar target telescope temperature tion transfer function transonic tube variable vehicle velocimeter velocity weight wind tunnel wing