Libros sobre el tema "Helicopter dynamic systems"

Jorgensen, Charles C. Analysis of tasks for dynamic man/machine load balancing in advanced helicopters. Oak Ridge, Tenn: Oak Ridge National Laboratory, 1987.

P, Townsend Dennis, Oswald Fred B y United States. National Aeronautics and Space Administration., eds. Experimental and analytical evaluation of dynamic load and vibration of a 2240-kW (3000-hp) rotorcraft transmission. [Washington, DC: National Aeronautics and Space Administration, 1987.

P, Townsend Dennis, Oswald Fred B y United States. National Aeronautics and Space Administration., eds. Experimental and analytical evaluation of dynamic load and vibration of a 2240-kW (3000-hp) rotorcraft transmission. [Washington, DC: National Aeronautics and Space Administration, 1987.

United States. National Aeronautics and Space Administration., ed. Studies of the dynamics of the twin-lift system: Interim report. Princeton, NJ: Dept. of Mechanical and Aerospace Engineering, Princeton University, 1989.

L, Wilbur Matthew, U.S. Army Research Laboratory. y Langley Research Center, eds. Wind-tunnel evaluation of the effect of blade nonstructural mass distribution on helicopter fixed-system loads. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.

C, Curtiss H. y United States. National Aeronautics and Space Administration., eds. An analytic modeling and system identification study of rotor/fuselage dynamics at hover. [Washington, DC: National Aeronautics and Space Administration, 1993.

K, Remple Robert, ed. Aircraft and rotorcraft system identification: Engineering methods with flight test examples. 2^a ed. Reston, VA: American Institute of Aeronautics and Astronautics, 2012.

K, Remple Robert, ed. Aircraft and rotorcraft system identification: Engineering methods with flight-test examples aircraft and rotorcraft system identification engineering methods with flight-test examples. Reston, VA: American Institute of Aeronautics and Astronautics, 2006.

V, Cook M., Rycroft Michael J, Institute of Mathematics and its Applications. y Conference on Aerospace Vehicle Dynamics and Control (1992 : Cranfield Institute of Technology), eds. Aerospace vehicle dynamics and control: Based on the proceedings of a conference organized by the Institute of Mathematics and its Applications on aerospace vehicle dynamics and control, held at the Cranfield Institute of Technology, in September 1992. Oxford: Clarendon Press, 1994.

Boden, Fritz. Advanced In-Flight Measurement Techniques. Berlin, Heidelberg: Springer Berlin Heidelberg, 2013.

Modeling Control And Coordination Of Helicopter Systems. Springer, 2011.

Fua, Cheng-Heng, Shuzhi Sam Ge, Tong Heng Lee, Chang Chen y Beibei Ren. Modeling, Control and Coordination of Helicopter Systems. Springer, 2012.

Ge, Shuzhi Sam, Chang Chen y Beibei Ren. Modeling, Control and Coordination of Helicopter Systems. Springer, 2011.

Fua, Cheng-Heng, Shuzhi Sam Ge, Tong Heng Lee, Chang Chen y Beibei Ren. Modeling, Control and Coordination of Helicopter Systems. Springer New York, 2014.

An analytic modeling and system identification study of rotor/fuselage dynamics at hover. [Washington, DC: National Aeronautics and Space Administration, 1993.

Tischler, Mark y Robert Remple. Aircraft And Rotorcraft System Identification: Engineering Methods With Flight-test Examples (Aiaa Education Series). AIAA (American Institute of Aeronautics & Ast, 2006.

Quiet mode for nonlinear rotor models. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1990.

Kompenhans, Jürgen, Fritz Boden, Nicholas Lawson y Henk W. Jentink. Advanced In-Flight Measurement Techniques. Springer, 2016.