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2421. NASA Technical Note: FLUTTER SUPPRESSION USING ACTIVE CONTROLS BASED ON THE CONCEPT OF AERODYNAMIC ENERGY

by Nissim, E.

Material type: book Book Description: 112p.Publisher: Washington, D.C. NASA 1971Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).

2422. AIRCRAFT ASSESMENT AND ACCEPTANCE TESTING

by .

Material type: book Book Description: v.Publisher: Agard, England 1980Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: 629.1345 AI74] (1).

2423. NASA Technical Note [NASA TN D-5862]: Simulator study of the instrument landing approach of a heavy subsonic jet transport with an external-flow jet-flap system used for additional lift

by Washington. National Aeronautics and Space Administration (NASA) | Grantham, William D | Deal, Perry L | Sommer, Robert W.

Material type: book Book Description: 35p.Publisher: Washington NASA 1970Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).

2424. NASA Technical Note [NASA TN D-5865]: Phase interpolation circuits for scanning phased arrays

by Washington. National Aeronautics and Space Administration (NASA) | Mailloux, R. J.

Material type: book Book Description: 12p.Publisher: Washington NASA 1970Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).

2425. NASA Technical Note [NASA TN D-5868]: Performance of twin gyro attitude control system including passive compensation and nonlinear control law

by Washington. National Aeronautics and Space Administration (NASA) | Campbell, Richard A.

Material type: book Book Description: 98p.Publisher: Washington NASA 1970Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).

2426. NASA Technical Note [NASA TN D-5869]: Description and performance of the Saturn launch vehicle's navigation, guidance and control system

by Washington. National Aeronautics and Space Administration (NASA) | Haeussermann, Walter.

Material type: book Book Description: 44p.Publisher: Washington NASA 1970Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).

2427. NASA Technical Note : STABILITY AND CONTROL CHARACTERISTICS OF A 0.0667-SCALE MODEL OF THE FINAL VERSION OF THE NORTH AMERICAN X-15 RESEARCH AIRPLANE (CONFIGURATION 3) AT TRANSONIC SPEEDS

by Osborne, Robert S.

Material type: book Book Description: 102p.Publisher: Washington, D.C. NASA 1963Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).

2428. FORCE-TEST INVESTIGATION OF THE STABILITY AND CONTROL CHARACTERISTICS OF A 1/8-SCALE MODEL OF A TILT-WING VERTICAL-TAKE-OFF-AND-LANDING AIRPLANE [NASA TN D-44]

by Tosti, L. P.

Material type: book Book; Format: print ; Literary form: not fiction Description: 127p.Publisher: Washington, D.C. National Aeronautics and Space Administration 1960Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).

2429. NASA Technical Note [NASA TN D-2596]: Application of a bang-bang control system to two spinning space vehicles

by Washington. National Aeronautics and Space Administration (NASA) | Rempfer, Paul S | Suddath, Jerrold H.

Description: 24p.Publisher: Washington NASA 1965Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).

2430. NASA Technical Note [NASA TN D-6299]: Fixed-base simulator investigation of lightweight vehicles for lunar escape to orbit with kinesthetic attitude control and simplified manual guidance

by Washington. National Aeronautics and Space Administration (NASA) | Middleton, David B | Hurt, George J.

Material type: book Book Description: 38p.Publisher: Washington NASA 1971Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).

2431. NASA Memorandum [NASA MEMO 4-20-59A]: Static stability and control of canard configurations at mach numbers from 0.70 to 2.22- lateral-directional characteristics of an unswept wing and canard

by Washington. National Aeronautics and Space Administration (NASA) | Peterson, Victor L.

Material type: book Book Description: 32p.Publisher: Nasa, Washington, D.C. 1959Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).

2432. NASA Memorandum [NASA MEMO 4-21-59A]: Longitudinal stability and control characteristics at mach numbers from 0.70 to 2.22 of a triangular wing configuration equipped with a canard control, a trailing-edge-flap control or a cambered forebody

by Washington. National Aeronautics and Space Administration (NASA) | Boyd, John W | Menees, Gene P.

Material type: book Book Description: 39p.Publisher: Washington NASA 1959Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).

2433. Flight Controllability limits and related human transfer functions as determined from simulator and flight tests

by Taylor, Lawrene W | Day, Richard E.

Material type: book Book; Format: print ; Literary form: not fiction Description: 65.Publisher: Washington D. C. Nasa, Washington, D.C. 1961Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-746] (1).

2434. NASA Technical Note [NASA TN D-5175]: An investigation of a direct side-force maneuvering system on a deflected jet VTOL aircraft

by Washington. National Aeronautics and Space Administration (NASA) | Feistel, Terrell W | Gerdes, Ronald M | Fry, Emmett B.

Material type: book Book Description: 14p.Publisher: Washington NASA 1969Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).

2435. DETERMINATION OF DYNAMIC PROCESSES IN PIECEWISE LINEAR AUTOMATIC CONTROL SYSTEMS [NASA TT F-132]

by Belya, K. K.

Material type: book Book; Format: print ; Literary form: not fiction Description: 21p.Publisher: Washington, D. C. National Aeronautics and Space Administration 1962Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).

2436. NASA Technical Note [NASA TN D-545]: A note on the drag due to lift of delta wings at mach numbers up to 2.0

by Washington. National Aeronautics and Space Administration (NASA) | Osborne, Robert S | Kelly, Thomas C.

Material type: book Book Description: 14p.Publisher: Washington NASA 1960Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).

2437. Experimental investigation of an attitude control system that uses star trackers and inertia wheels [NASA TN D-5843]

by Showman, Robert D | Dishman, Bruce H.

Material type: book Book; Format: print ; Literary form: not fiction Description: 36p.Publisher: Washington, D.C. Nasa 1970Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).

2438. NASA Technical Note : PNEUMATIC ARTIFICIAL HEART DRIVING SYSTEM PROVIDING QUASI-STEADY-STATE REGULATION AND PRESSURE WAVEFORM CONTROL.

by Webb, John A | Dustin, Miles O | Crosby, Michael J.

Material type: book Book Description: 26p.Publisher: Washington, D.C. NASA 1971Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).

2439. Measured human transfer functions in simulated single-degree-of -freedom nonlinear control systems. [ NASA TN D-2571]

by Bergeron, Hugh P | Adams, James J | Joseph, K. Kincaid.

Material type: book Book; Format: print ; Literary form: not fiction Description: 42p.Publisher: Washington, D.C. Nasa 1965Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-2571] (1).

2440. NASA Technical Note [NASA TN D-5049]: Fixed-base visual simulation of pilot-controlled descents of an advanced Apollo spacecraft with an all-flexible parawing

by Washington. National Aeronautics and Space Administration (NASA) | Miller, G. Kimball | Jaquet, Byron M | Price, Douglas B.

Material type: book Book Description: 61p.Publisher: Washington NASA 1969Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).

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