Books on the topic '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, and 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, and 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., and 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., and 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. 2nd 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., and 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, and Beibei Ren. Modeling, Control and Coordination of Helicopter Systems. Springer, 2012.

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

Fua, Cheng-Heng, Shuzhi Sam Ge, Tong Heng Lee, Chang Chen, and 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, and 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, and Henk W. Jentink. Advanced In-Flight Measurement Techniques. Springer, 2016.