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ATTITUDE CONTROL REQIREMENTS FOR HOVERING DETERMINED THROUGH THE USE OF A PILOTED FLIGHT SIMULATOR

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BookPublisher: Nasa, Washington, D.C. 1961Description: 20.DDC classification: NASA | TN D-792 -

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Item type	Current location	Collection	Call number	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	General Stacks	NASA TN D-792 - (Browse shelf)	Not for loan		TR8251

Total holds: 0

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Previous	NASA TN D-778 A FLIGHT STUDY OF THE DYNAMIC STABILITY OF A TILTING-ROTOR CONVERTIPLANE	NASA TN D-779 FLIGHT INVESTIGATION USING VARIABLE-STABLITY AIRPLANES OF MINIMUM STABILITY REQUIREMENTS FOR HIGH-SPEED, HIGH-ALTITUDE VEHICLES	NASA TN D-780 A METHODS FOR OBTAINING THE NONLINEAR AERODYNAMIC STABILITY CHARACTERISTICS OF BODIES OF REVOLUTION FROM FREE-FLIGHT TESTS	NASA TN D-792 - ATTITUDE CONTROL REQIREMENTS FOR HOVERING DETERMINED THROUGH THE USE OF A PILOTED FLIGHT SIMULATOR	NASA TN D-802 A PRELIMINARY INVESTIGATION OF THE EFFECT OF BUMPERS AS A MEANS OF REDUCING PROJECTILE PENETRATION	NASA TN D-803 EFFECTS OF MASS-LOADING VARIATIONS AND APPLIED MOMENTS ON MOTION AND CONTROL OF A MANNED ROTATING SPACE VEHICLE	NASA TN D-804 INVESTIGATION AT HIGH SUBSONIC SPEEDS OF THE USE OF LOW AUXILIARY TAIL SURFACES HAVING DIHEDRAL TO IMPROVE THE LONGITUDINAL AND DIRECTIONAL STABILITY OF A T-TAIL MODEL AT HIGH LIFT	Next

Bound With Nasa Tn D-792-800

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