Authors A.A. Kolesnikov, E.S. Kreerenko, O.S. Dinchari
Month, Year 07, 2015 @en
Index UDC 681.51
Abstract Main task of modern aerospace industry is delivery of heavy vehicles to the orbit. The preferred and economical is launching spacecraft from the spaceports near the equator. Basing on experience, the launch of carrier rocket from floating platform «Marine launch» might constitute a serious threat to World’s ocean in case of faulty launch. Launching spacecraft by aerospace system of air start near equator which based on super-heavy amphibious aircraft is more referenced from economical point of view. Aerospace system consists of launch aircraft, upper-stage rocket and spaceplane. The new approach to synthesis of control laws of aviation-airspace system based on nonlinear dynamics procedures is considered in the given paper. There is used the synergetic method of analytical designing of aggregated regulators (ADAR) to synthesize the basic control laws. In accordance with the object view there are solved following tasks: synthesize control laws, which providing lift of lunch aircraft at predetermined altitude and desirable airspeed; upper-stage rocket separating from launch aircraft; reaching hypervelocity acceleration. The task is implemented in software «Maple». While computer modeling control laws provides asymptotic stability of closed nonlinear system and achievement of predetermined technologic invariant.

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Keywords Aerospace system; synthesis of control laws; invariant manifold; functional equation.
References 1. Chernyy I. Vozdushnyy start 2009 [Air launch 2009], Novosti kosmonavtiki [News of Cosmonautics], 2009, No. 5, pp. 15.
2. Afanas'ev I.B. Hotol angliyskiy. Tri poteryannykh klyucha [Hotol English. Three lost key], Novosti kosmonavtiki [News of Cosmonautics], 2008, No. 9, pp. 49-53.
3. Afanas'ev I.B. Saenger nemetskiy. Tri poteryannykh klyucha [Saenger German. Three lost key], Novosti kosmonavtiki [News of Cosmonautics], 2008, No. 6, pp. 50-57.
4. Afanas'ev I.B. «Vozdushnyy start» poamerikanski ["Air launch" American], Novosti kosmonavtiki [News of Cosmonautics], 2006, No. 1, pp. 49-54.
5. Dornheim M.A. New path to space?, Aviation week and space technology, 2005, No. 10, pp. 40.
6. Linehan D. SpaceShipOne: An Illustrated History. Colorado: Zenith Press, 2008, 160 p.
7. Sarigul-Klijn M., Sarigul-Klijn N., Hudson G. Flight Testing of a Gravity Air Launch Method to Enable Responsive Space Access., 2007. 20 p. (AIAA paper 2007-6146).
8. Hampsten K.R., Walker J.M. BladeRunner Aerospace Vehicle, Space Station Service Vehicles Conf AIAA Intl. Orlando: AIAA, 2009, pp. 56.
9. Kolesnikov A.A. Sinergeticheskaya teoriya upravleniya [Synergetic control theory]. M.: Energoatomizdat, 1994, 344 p.
10. Veselov G.E. Cinergeticheskiy podkhod k sintezu ierarkhicheskikh sistem upravleniya [A synergistic approach to the synthesis of hierarchical control systems], Izvestiya TRTU [Izvestiya TSURe], 2006, No. 6 (61), pp. 73-84.
11. Sovremennaya prikladnaya teoriya upravleniya. Ch. II: Sinergeticheskiy podkhod v teorii upravleniya [Modern applied control theory. Part II: Synergetic approach in control theory], By ed. A.A. Kolesnikova. Moscow-Taganrog: Izd-vo TRTU, 2000.
12. Kolesnikov A.A., Veselov G.E., Popov A.N., Mushenko A.S. i dr. Sinergeticheskie metody upravleniya slozhnymi sistemami: mekhanicheskie i elektromekhanicheskie sistemy [Synergetic control methods of complex systems: mechanical and Electromechanical systems]. Moscow: KomKniga, 2006, 304 p.
13. Kolesnikov A.A. Introduction of synergetic control, Proceedings of the American Control Conference ACC-2014, Portland, OR, USA, 4-6 June 2014, pp. 3013-3016.
14. Veselov G.E., Popov А.N., Radionov I.A., Mushenko A.S. Adaptive Power Saving Control for Traction Asynchronous Electrical Drive: Synergetic Approach, Proc. of IEEE «EnergyCon 2014», Dubrovnik, Croatia, 13-16 May 2014, pp. 1446-1453.
15. Popov Andrey, Radionov Ivan, Mushenko Alexey. Synergetic synthesis of power saving control for locomotive asynchronous drive systems, Proceedings of 6th ICUMT-2014, 6-8 October 2014, St. Petersburg, Russia, pp. 546-550.
16. Kreerenko Evgeny. Synthesis of Control Laws Sea Launch Aerospace System on the Basis of Super-heavy Amphibian Aircraft, Proceedings CHAOS2014 Conference, June 7–10, 2014, Lisbon, Portugal, 2014, pp. 39-47.
17. Kobzev V.A., Fortinov L.G., Glombinskiy E.N. Kompleksnaya sistema dlya zapuska tyazhelykh vozdushno-kosmicheskikh samoletov mnogorazovogo ispol'zovaniya na okolozemnuyu orbitu, supertyazhelyy reaktivnyy samolet-amfibiya dlya nee (varianty) i sposob osushchestvleniya zapuska [A comprehensive system to run heavy aerospace aircraft reusable
in earth orbit, heavyweight jet amphibian aircraft for it (versions) and method of implementation of the launch]. Patent RF, No. 2397922, priority from 30.07.2008.
18. Byushgens G.S., Studnev R.V. Aerodinamika samoleta: Dinamika prodol'nogo i bokovogo dvizheniya [Aerodynamics of the airplane: longitudinal and lateral Dynamics of the movement]. Moscow: Mashinostroenie, 1979, 352 p.
19. Krasovskiy N.N. Teoriya upravleniya dvizheniem [Theory of motion control]. Moscow: Nauka, 1968, 475 p.
20. Meshcherskiy I.V. Raboty po mekhanike tel peremennoy massy [Works on mechanics of bodies of variable mass]. 2nd ed. Moscow: GITTL, 1952, 281 p.

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