PERFORMANCE CRITERION OF A TRANSIENT PROCESS AND ACCURACY FIGURES OF A ROCKET STABILIZATION SYSTEM

Вольт Васильевич Авдеев

Abstract


Equations given connection between criteria coefficients, control law, coordinates vectors of errors and the work of an inertial actuating link during transient process of a constant disturbing acceleration compensation for the case of a plain rotation movement are obtained. Unlike traditional form of a control law that in article takes in account all coordinates of the state vector according to chosen model what has a positive influence on stability factor and stabilization accuracy. Obtained results give the possibility to determine control law coefficients on the assumption of taken priority system’s indexes.


Keywords


transient process; control law; accuracy; work of executive devices

References


Kolesnikov, K. S. Dinamika raket [Missile Dynamics]. Mokow, Mashinostrojenie Publ., 1980, 376 p.

Igdalov I. M., Kutchma, L. D., Poljakov, N. V., Sheptun, Ju. D. Dinamitcheskoje proektirovanie raket. Zadatchi dinamiki raket i kosmitcheskych stupenej [Dynamic design rockets. The objectives of the dynamics of rockets and space stages]. Dnepr, Izd-vo Dnjepropetr. naz. un-ta Publ., 2010. 264 p.

Kuzovkov, N. T. Systemy stabilizazii letatelnych apparatov (ballistitcheskych i zenitnych raket) [Systems of aircraft stabilization (ballistic and anti-aircraft missiles)]. Moskow, Vysshaja shk. Publ., 1976. 364 p.

Avdejev, V. V. Zapas ustoitchivosti systemy stabilizazii vrashtchatelnogo dvizgenia rakety [Margin of stability of the rotational motion of the rocket stabilization systems]. Technitcheskaja mechanika, no. 4, 2016, pp. 62 – 69.

Ajzenberg, J. E., Suchorebry, V. G. Proektirovanie system stabilizazii nositelej kosmitcheskych apparatov [Designing Media stabilization systems]. Moskow, Mashinostrojenie Publ., 1986. 224 p.

Avdejev, V. V. Koeffizienty oshibok stabilizazii vrashtchatelnogo dvizgenia raket [Odds error rotational movement of a rocket stabilization]. Technitcheskaja mechanika, no. 3, 2014, pp. 71-78.

Avdejev, V. V. Totchnist i zapas stijcosti systemy stabilizazii obertalnogo ruchu rakety [Accuracy and stability of the stabilization reserve rotational motion missiles]. Radioelektronika, informatyka, upravlinnja, 2016, no. 3, pp. 93-98.

Krasovsky A. A. Analititcheskoje konstruirovanie konturov upravlenija letatelnymi apparatami [Analytical design of aircraft control loops]. Moskow, Mashinostrojenie Publ., 1969. 240 p.

Avdeyev V. Transient process at satellite angular position stabilization. Proceedings of 5th intern. conf. “Space technologies: present and future”, Dnepropetrovsk, May 2015, pp. 102.

Sheptun, Ju. D., Kovalenko, T.O. Analiz vytrat energii na keruvannja kosmitchnym stupenem rakety [Cost analysis of energy management level space rocket]. Visnyk DNU, no. 4, vol. 24, Seria «Raketnokosmitchna technika», 2016, vyp. 19, pp. 145-157.

Krasovskiy, A. A. Spravotchnik po teorii avtomatitcheskogo upravlenija [Guide to automatic control theory]. Moskow, Nauka Publ., 1987. 712 p. Поступила в редакцию 23.01.2017, рассмотрена на редколлегии 15.02.2017.




DOI: https://doi.org/10.32620/aktt.2017.1.01