Abstract Algorithms for constructing parametric vector functions are considered to determine flight trajectories in the design calculations of flight vehicle weight parameters and flight characteristics, in the calculations of stability and required aerodynamic moments of the controlling and stabilizing surfaces when flying over the specified trajectory leg.
Design calculation of light piston-engined aircraft controllability and stability parameters
Russian Aeronautics (Iz VUZ) ; 53 , 2 ; 134-140
2010-06-01
7 pages
Article (Journal)
Electronic Resource
English
Design calculation of light piston-engined aircraft controllability and stability parameters
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