Active control of vibrations of gyroscope on rocket deck

• Autorzy: Koruba, Z. , Krzysztofik, I.
• Języki publikacji: EN

Abstrakty

EN

The paper discusses errore of astatic gyroscope, located on board of a homing missile, suspended on Cardan joint. The impact of friction in suspension bearings, the base kinematic input and linear accelerations on the gyroscope axis position are also investigated. The paper gives the algorithm for the optimum correction control. Its role is to minimise the impact of rocket vibrations and manoeuvres on the gyroscope work accuracy.

Słowa kluczowe

EN

homing missile; gyroscope; dynamics; control; optimisation

• Czasopismo: Archives of Control Sciences
• Rocznik: 2003
• Tom: Vol. 13, no. 3
• Strony: 313-326
• Opis fizyczny: Bibliogr. 6 poz., rys.

Twórcy

autor

Koruba, Z.

• Faculty of Mechatronics and Machine Building, Kielce University of Technology, Kielce, Poland,

autor

Krzysztofik, I.

• Faculty of Mechatronics and Machine Building, Kielce University of Technology, Kielce, Poland

Bibliografia

• [1] R. Grammel: Der Kreisel Seine Theorie und Seine Anwendungen. Zweiter Band: Die Anwendugen des Kresels, 1950.
• [2] Z. Koruba: Dynamics and Control of Gyroscope on the Board of Aerial Vehicle. Monographs, Studies, Dissertations No 25. Kielce University of Technology, Kielce 2001, p. 285 (in Polish).
• [3] Z. Koruba and J. Osiecki: Construction, Dynamics and Navigation of Close-Range Missiles - part I. University course book no 348, Kielce University of Technology Publishing House, Kielce 1999, PL ISSN 0239-6386, p. 168 (in Polish).
• [4] K. Magnus: Kreisel. Theorie und Anwendungen. Springer-Verlag, Berlin-Heidelberg-New York, 1971.
• [5] V.A. Pavlov: Gyroscope units for aerial vehicles. Nat. Publ. of Defense Industry. Moscow, 1954, (in Russian).
• [6] M.A. Pavlovskij: Theory of gyroscopes. Higher School Publ. Kiyev, 1986, (in Russian).