Abstract
The problem of attitude control of a gyro-stabilized platform with the structurally uncertain drift model is solved. The solution is realized in two stages. At the first stage, on the basis of the obtained stochastic model of the reusable spacecraft navigation system, the drift model of gyro-stabilized platform is identified. At the second stage, the control of its spatial orientation is synthesized with regard to the found drift model. The results of numerical simulation are presented in conclusion.
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Razorenov, G.N., Bakhramov, E.A., and Titov, Yu.F., Sistemy upravleniya letatel’nymi apparatami (Control Systems for Flying Vehicles), Moscow: Mashinostroenie, 2003.
Pupkov, K.A. and Neusypin, K.A., Voprosy teorii i realizatsii sistem upravleniya i navigatsii (Systems of Control and Navigation: Issues of Theory and Implementation), Moscow: Bioinform, 1997.
Ishlinskii, A.Yu., Orientatsiya, giroskopy i inertsial’naya navigatsiya (Attitude Control, Gyroscopes, and Inertial Navigation), Moscow: Nauka, 1976.
Wrigley, W., Denhard, W.G., and Hollister, W.M., Gyroscopic Theory, Design, and Instrumentation, The MIT Press, 1969. Translated under the title Teoriya, proektirovanie i ispytanie giroskopov, Moscow: Mir, 1972.
Bel’skii, L.N., and Vodicheva, L.V., Rapid High-Precision Initial Adjustment and Calibration of Inertial Navigation System of a Flying Vehicle with Movable Platform, Giroskopiya i Navigatsiya, 2001, no. 4 (35).
Dzhashitov, V.E., and Pankratov, V.M., Matematicheskie modeli teplovogo dreifa giroskopicheskikh datchikov inertsial’nykh sistem (Mathematical Models of Thermal Drift for Gyroscopic Sensors of Inertial Systems), St. Petersburg: RF State Research Center TsNII Elektropribor, 2001.
Khutortsev, V.V., Sokolov, S.V., and Shevchuk, P.S., Sovremennye printsipy upravleniya i fil’tratsii v stokhasticheskikh sistemakh (Modern Principles of Control and Filtering in Stochastic Systems), Moscow: Radio i Svyaz’, 2001.
Branets, V.N. and Shmyglevskii, I.P., Primenenie kvaternionov v zadachakh orientatsii tverdogo tela (Application of Quaternions in Problems of Solid Body Attitude Control), Moscow: Nauka, 1979.
Sokolov, S.V. and Polovinchuk, N.Ya., Teoreticheskie osnovy sinteza avtonomnykh pomekhoustoichivykh besplatformennykh navigatsionnykh sistem (Theoretical Principles of Synthesizing Autonomous Noise-Immune Platformless Navigation Systems) Rostov-on-Don: MO RF, 1997.
Shannon, C.E., Raboty po teorii informatsii i kibernetike (Papers on Information Theory and Cybernetics), Moscow: Izd. Inostr. Lit., 1961.
Stratonovich, R.L., Uslovnye Markovskie protsessy i ikh primenenie k teorii optimal’nogo upravleniya (Conditional Markovian Processes and Their Application to Optimal Control Theory), Moscow: Izd. Mosk. Gos. Univ., 1966.
Chernov, A.A. and Yastrebov, V.D., Perturbations in the Process of Kalman Filtering, Kosm. Issled. (Cosmic Res.), 1984, vol. 22, no. 4, pp. 537–542.
Kazakov, I.E., Optimization of Control in Nonlinear Stochastic System according to Local Criterion, Izv. Ross. Akad. Nauk, Teor. Sist. Upr., 1996, no. 6.
Kazakov, I.E., Analytical Design of Conditionally Optimal Control in Nonlinear Stochastic System according to Local Criterion, Izv. Ross. Akad. Nauk, Teor. Sist. Upr., 1994, no. 1.
Sokolov, S.V. and Kramarov, S.O., Volnovodnaya vychislitel’naya optika (Waveguide Computational Optics), Rostov-on-Don: MO RF, 1999.
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Original Russian Text © V.A. Pogorelov, 2009, published in Kosmicheskie Issledovaniya, 2009, Vol. 47, No. 1, pp. 55–63.
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Pogorelov, V.A. Application of information criteria to control the structurally uncertain navigation system of a reusable spacecraft. Cosmic Res 47, 44–52 (2009). https://doi.org/10.1134/S0010952509010067
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DOI: https://doi.org/10.1134/S0010952509010067