APPLICATION OF DIFFERENTIAL TRANSFORMATIONS FOR THE MODELING MOTION OF AEROSTATIC VEHICLES AND FOR THE SYNTHESIS OF CONTROL ALGORITHMS

Authors

  • A.V. Gusynin NAU Aerospace Institute

DOI:

https://doi.org/10.18372/2306-1472.24.1151

Abstract

 The approach to simulation of flight dynamics and numerically-analytical method of airship control algorithms are offered. It’s based on differential transformations of initial mathematical model of airship motion. The given approach allows for elimination of viewing time function for their differential spectra in the image field. It gives the possibility to reduce a problem of closed algorithm synthesis of vehicle control to the solution of non-linear equation system concerning control variable.

References

Nagabhushan B.L., Faiss G.D. Thrust vector of a V/STOL airship // Journal of aircraft. – 1984. – Vol. 21, №6. – P. 408–413.

Nagabhushan B.L., Tomlinson N.P. Thrust-vectored takeoff, landing and ground handling of an airship //Journal of aircraft. – Vol. 23, №3. – 1985. – P. 250–256.

Gusynin V.P., Baranov V.L., Gusynin A.V. Synthesis of control of the ascent into orbit of multimode aerospace systems // Proc. of AAS/AIAA Astrodynamics specialists conf. – Quebec City, Quebec. – Canada. –Jul. 30 – Aug. 02, 2001. – P. 50–60.

Пухов Г.Е. Дифференциальные спектры и модели. – К.: Наук. думка, 1990. – 180 с.

Сейдж Э.П., Уайт Ч.С. Оптимальное управление системами. – М.: Радио и связь, 1982. – 350 c.

Диференціальні перетворення в задачах керування рухом літальних апаратів: Навч. посіб./ В.Л. Баранов, В.П. Гусинін, А.В. Гусинін та ін. – К.: НАУ. – 2003. – 158 с.

Уруский О.С., Баранов В.Л. Синтез замкнутых законов терминального управления на основе дифференциальных преобразований // Электронное моделирование. – 1996. – 18, №3. – С. 3–8.

Jones S.P., Krausman J.A. Nonlinear Dynamic simulation of tethered aerostat//Journal of aircraft. – 1982. –Vol. 19. – P. 679–686.

Jones S.P., DeLaurier J.D. Aerodynamic estimation techniques for aerostat and airship//Journal of aircraft. – 1983. – Vol. 20. – P. 120–126.

Jones R. Acceleration derivatives in the gase of a body moving in an ideal fluid // ARC R&M 748. –Apr., 1921. – Р. 45–54.

Гусынин В.П., Гусынин А.В. Системоаналоговое моделирование процесса управления дирижаблем с отклоняемым вектором тяги // Тр. конф. «Dynamical systems modeling and stability investigation». – К. , 2001. – С. 164.

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How to Cite

Gusynin, A. (2005). APPLICATION OF DIFFERENTIAL TRANSFORMATIONS FOR THE MODELING MOTION OF AEROSTATIC VEHICLES AND FOR THE SYNTHESIS OF CONTROL ALGORITHMS. Proceedings of National Aviation University, 24(2), 83–88. https://doi.org/10.18372/2306-1472.24.1151

Issue

Section

AEROSPACE SYSTEMS FOR MONITORING AND CONTROL