SYNTHESIS OF KINEMATIC CONTROL OF AN AIRCRAFT IN ”BIG”
DOI:
https://doi.org/10.18372/2306-1472.58.6664Keywords:
aircraft, autonomy, bifurcation, invariance, nonlinear object, reconfiguration technologyAbstract
In the article the application reconfiguration technology for the decision of a problem of difficult nonlinear object control in the greatest possible area of its states is shown.References
Casanova, V. ; Salt, J. Multirate control implementation for an integrated communication and control system. Control Engineering Practice. 2003. Vol. 11. P 1335–1348.
Daryin, A.N.; Kurzhanski, A.B. Nonlinear Control Synthesis under Double Constraints. Proceedings of 16th World Congress IFAC. Prague, Czech. 2005. 6 р.
Devis, R. The human operator us a single channel information system. Quarterly journal of experi¬mental psychology. 1957. Vol 9, N 3. P. 119–129.
Dynamics of maneuverable aircrafts on modes of flight with the big angles of attack. Review of Branch of the Scientific and technical Information of the Central Aerohydrodynamic Institute. Moscow. 1979. N 558. 124 p. (in Russian).
Gorbatenko, S.A.; Makashov, E.M.; Polushkin, Yu.F.; Sheftel, L.V. Calculation and the analysis of aircrafts motion. Engineering Handbook. Moscow, Mashynostroenie. 1971. 352 p. (in Russian).
Krotov, V.F.; Kurzhanski, A.B. National Achievements in control theory (The Aerospace Perspective). 2004. Electronic resource. Available from Internet: <http://aca2004.aanet.ru.004.pdf>.
Mс. Ruer, D.T.; Сrendel, E.S. The Man-machine System Conception. Proceedings Institute Radio Engrs. 1962. N 5. P. 23-29.
Ostoclavskiy, I.V.; Strazheva, I.V. Dynamics of flight. An aircrafts trajectory. Moscow, Mashynostroenie. 1969. 499 p. (in Russian).
Pavlov,V.V. The beginnings of ergatic systems theory. Kyiv, Naukova Dumka. 1975. 240 p. (in Russian).
Pavlov, М.V.; Pavlova, S.V. Concept “a phase of a differential cone of inclusion”. Cybernetics and computer facilities. 2003. Release 140. P. 3–11. (in Russian).
Pavlov, V.V.; Pavlova, S.V. Phase analysis of vector fields of dynamic systems of balance type. Cybernetics and computer facilities. 2003. Release 141: P. 58–69. (in Russian).
Pavlova, S.V. Bifurcation property of control functions of aircrafts. Materials of VІII international scientific and technical conference “AVIA-2007”. 2007. Vol. 1. P. 21.52–21.54 (in Russian).
Pavlova, S.V. Model of cones of aircraft motion. Proceedings of the National Aviation University. 2003. N 3-4. P. 89–92 (in Ukrainian).
Pavlova, S.V. Topological estimation of functionality of controlled aerodynamic aircraft system quality. Proceedings of the National Aviation University. 2005. N 1. P. 48–54 (in Ukrainian).
Salt, J.; Albertos, P. Model–based multirate controllers design. IEEE Transactions on Control Systems Technology. 2005. Vol. 13. N. 6. P. 988–997.
Daryin, A.N.; Kurzhanski, A.B. Nonlinear Control Synthesis under Double Constraints. Proceedings of 16th World Congress IFAC. Prague, Czech. 2005. 6 р.
Devis, R. The human operator us a single channel information system. Quarterly journal of experi¬mental psychology. 1957. Vol 9, N 3. P. 119–129.
Dynamics of maneuverable aircrafts on modes of flight with the big angles of attack. Review of Branch of the Scientific and technical Information of the Central Aerohydrodynamic Institute. Moscow. 1979. N 558. 124 p. (in Russian).
Gorbatenko, S.A.; Makashov, E.M.; Polushkin, Yu.F.; Sheftel, L.V. Calculation and the analysis of aircrafts motion. Engineering Handbook. Moscow, Mashynostroenie. 1971. 352 p. (in Russian).
Krotov, V.F.; Kurzhanski, A.B. National Achievements in control theory (The Aerospace Perspective). 2004. Electronic resource. Available from Internet: <http://aca2004.aanet.ru.004.pdf>.
Mс. Ruer, D.T.; Сrendel, E.S. The Man-machine System Conception. Proceedings Institute Radio Engrs. 1962. N 5. P. 23-29.
Ostoclavskiy, I.V.; Strazheva, I.V. Dynamics of flight. An aircrafts trajectory. Moscow, Mashynostroenie. 1969. 499 p. (in Russian).
Pavlov,V.V. The beginnings of ergatic systems theory. Kyiv, Naukova Dumka. 1975. 240 p. (in Russian).
Pavlov, М.V.; Pavlova, S.V. Concept “a phase of a differential cone of inclusion”. Cybernetics and computer facilities. 2003. Release 140. P. 3–11. (in Russian).
Pavlov, V.V.; Pavlova, S.V. Phase analysis of vector fields of dynamic systems of balance type. Cybernetics and computer facilities. 2003. Release 141: P. 58–69. (in Russian).
Pavlova, S.V. Bifurcation property of control functions of aircrafts. Materials of VІII international scientific and technical conference “AVIA-2007”. 2007. Vol. 1. P. 21.52–21.54 (in Russian).
Pavlova, S.V. Model of cones of aircraft motion. Proceedings of the National Aviation University. 2003. N 3-4. P. 89–92 (in Ukrainian).
Pavlova, S.V. Topological estimation of functionality of controlled aerodynamic aircraft system quality. Proceedings of the National Aviation University. 2005. N 1. P. 48–54 (in Ukrainian).
Salt, J.; Albertos, P. Model–based multirate controllers design. IEEE Transactions on Control Systems Technology. 2005. Vol. 13. N. 6. P. 988–997.
Downloads
Published
25-06-2014
How to Cite
Pavlova, S. (2014). SYNTHESIS OF KINEMATIC CONTROL OF AN AIRCRAFT IN ”BIG”. Proceedings of National Aviation University, 58(1), 17–25. https://doi.org/10.18372/2306-1472.58.6664
Issue
Section
AEROSPACE SYSTEMS FOR MONITORING AND CONTROL
