Sudars, M. (2009). Development and simulations of aircraft guidance system using a 3-degree-of-freedom point mass model. Aviation (Vilnius, Lithuania), 13(2), 35-43. https://doi.org/10.3846/1648-7788.2009.13.35-43
Citace podle Chicago (17th ed.)Sudars, Martins. "Development and Simulations of Aircraft Guidance System Using a 3-degree-of-freedom Point Mass Model." Aviation (Vilnius, Lithuania) 13, no. 2 (2009): 35-43. https://doi.org/10.3846/1648-7788.2009.13.35-43.
Citace podle MLA (9th ed.)Sudars, Martins. "Development and Simulations of Aircraft Guidance System Using a 3-degree-of-freedom Point Mass Model." Aviation (Vilnius, Lithuania), vol. 13, no. 2, 2009, pp. 35-43, https://doi.org/10.3846/1648-7788.2009.13.35-43.
Upozornění: Tyto citace jsou generovány automaticky. Nemusí být zcela správně podle citačních pravidel..