Abstract
An algorithm is proposed for computer-aided calculation of required values of aircraft controlling moments and aerodynamic moment coefficients for stable fulfillment of flight trajectories specified by design flight performance.
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Original Russian Text © V.G. Gainutdinov, 2010, published in Izvestiya VUZ. Aviatsionnaya Tekhnika, 2010, No. 3, pp. 24–27.
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Gainutdinov, V.G. An algorithm for computer-aided design calculation of aircraft stability and controllability parameters. Russ. Aeronaut. 53, 277–282 (2010). https://doi.org/10.3103/S1068799810030062
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DOI: https://doi.org/10.3103/S1068799810030062