Flight Dynamics Principles: A Linear Systems Approach to Aircraft Stability and Control
By M. Cook. 2007
280 citations recorded by the source corpus.
View Paper: https://www.semanticscholar.org/paper/3cebdd9a69951a64d7694b166a3ef3c49503a263
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Citations in the corpus
- Applications of the unsteady vortex-lattice method in aircraft aeroelasticity and flight dynamics (2012, background): “These are typically pre-computed for a variety of flight and control states and are tabulated in databases [159].”
- Applied Tracking Control for Kite Power Systems (2014, background): “In aerospace engineering, it is common practice to describe the attitude of airplanes using XYZ-type Eulerangles [19] between a NED-type (north-east-down) earth-fixed reference frame and the body-fixed reference frame of the flying vehicle.”