Book Chapters:

 

Goman, M.G., Khramtsovsky, A.V. and Kolesnikov, E.N. (2007) Chapter 13 Investigation of the ADMIRE Manoeuvring Capabilities Using Qualitative Methods in Book Nonliner Analysis and DesignMethods in Aircraft Control, Martin Hagstrom and Declan Bates, Editors, Springer, pp. 301-324.

 

Sidoryuk, M.E., Goman, M.G., Kendrick, S., Walker, D.J. and Perfect, P. (2007) Chapter 10 An LPV Control Law Design and Evaluation for the ADMIRE Model in Book Nonliner Analysis and Design Methods in Aircraft Control, Martin Hagstrom and Declan Bates, Editors, Springer, 2007, pp.197-229.

 

Goman, M.G. and Demenkov, M.N. (2004) Chapter 8 Stabilization of unstable aircraft dynamics under control constraints in Book Advances in Dynamics and Control Volume 2 in series Nonlinear Systemsin Aviation, Aerospace, Aeronautics and Astronautics, Sivasundaram S., Editor, CRC Press,USA, pp. 344 - 357.

 

Goman, M.G., Khrabrov, A.N., and Khramtsovsky, A.N. (2002).Chaotic Dynamics in a Simple Aeromechanical System in Book Fractal Geometry: Mathematical Methods, Algorithms, Applications, J.M.Blackledge, A.K.Evans and M.J.Turner, Editors, Horwood Publishing Series in Mathematics and Applications, pp. 1-15.

Goman, M.G.(2002) Chapter 2.1 Flight mechanics principles in Mechanical Engineering Encyclopedia, Vol.IV-21, Book 1 Aerodynamics, Flight Dynamics and Strength, Bushgens, G.S., Editor, Mashinostroenie, Moscow, 799pp, pp. 276-313.

 

Goman, M.G. (1998): Chapter 8 Manoeuvring aerodynamics of supersonic aircraft;

Chapter 10 Basic methods of analysis in flight dynamics;

Chapter 15 Dynamics of spatial aircraft motion

in Book "Aerodynamic, Stability & Controllability of Supersonic Aircraft", Bushgens, G.S., Editor, Nauka Fizmatlit, Moscow, 811 pp.

 

Refereed Journal Papers:

Goman, M.G., Khramtsovsky, A.V., & Kolesnikov, E.N., Evaluation of Aircraft Performance and Maneuvrability by Computation of Attainable Equilibrium Sets AIAA Journal of Guidance, Control, and Dynamics (accepted for publication).

 

Goman, M.G. & Khramtsovsky, A.N. (2008) Computational framework for Investigation of Aircraft Nonlinear Dynamics. Journal Advances in Engineering Software, Volume 39, Issue 3, pp.167-177, doi:10.1016/j.advengsoft.2007.02004

 

Goman,M.G., Sidoryuk, M.E., and Khrabrov, A.N. (2006) On Unsteady Aerodynamic Airfoil Loads in the Design of a Control System for Minimizing the Effect of Wind Perturbations Using the Rudder on the Trailing Edge of the Wing. Journal of Computer and Systems Sciences International, 2006, Vol.45, No.5, pp.812-823. ISSN 1064-2307, Pleiades Publishing, Inc.

 

Goman, M.G. & Demenkov, M.N. (2004) Computation of Controllability Regions for Unstable Aircraft Dynamics. Journal of Guidance, Control, and Dynamics 27, (4), 213{224.

 

Goman, M.G. & Khramtsovsky, A.V. (1998) Application of Bifurcation and Continuation Methods for an Aircraft Control Law Design. In the Theme Issue Flight Dynamics of High Performance Manoeuvrable Aircraft. Phil. Trans. Roy. Soc. Lond. A 356, 2277-2295.

 

Goman, M.G., Zagainov, G.I. & Khramtsovsky, A.V. (1997) Application of Bifurcation Methods to Nonlinear Flight Dynamics Problems. Progress in Aerospace Sciences 33, pp. 539-586, Elsevier Sciences, Ltd.

 

Goman, M.G., Matiukhin, V.I. & Pyatnitsky, E.S. (1996) Attitude control of solid body moving in an aerodynamic media. Dokl. Akad. Nauk of Russia 343, (3).

 

Bushgens, G.S., Goman, M.G., Matiukhin, V.I. & Pyatnitsky, E.S. (1995) Stabilazibility and universal control laws for solid body motion taking into account aerodynamic effects. Dokl. Akad .Nauk of Russia. 342, (1), pp. 49-52.

 

Goman, M.G., Usoltsev, S.P. & Khrabrov, A.N. (1995) Dynamics of an Aircraft Movable in Bank and Yaw Model in a Wind Tunnel. Uch. Zap. TsAGI. 26, (3-4), pp. 75-85.

 

Goman, M.G., Kolesnikov, E.N. & Usoltsev, S.P. (1995) Aircraft Model Dynamics on Pendulum Suspension in Wind Tunnel Flow. Uch. Zap. TsAGI. 26, (3-4), pp. 65-74.

 

Goman, M.G. & Khramtsovsky, A.V. (1994) Analysis of the Asymptotic Stability Region Boundary for a Dynamic System. The TsAGI Journal 1 (1), pp. 25-54.

 

Goman, M.G. & Khrabrov, A.N. (1994) State-Space Representation of Aerodynamic Characteristics of an Aircraft at High Angles of Attack. Journal of Aircraft 31, (5), pp.1109-1115.

 

Bushgens, G.S, Goman, M.G., Matukhin, V.I. & Pyatnitsky, E.S. (1992) Lyapunov function method in problems of control law design for aircraft spatial motion. Preprint of Inst. of Control Sci.RAS.

 

Goman, M.G. & Ahrameev, V.I. (1991) Automatic control for aircraft recovery from spin. Technika Vozdushnogo Flota (No. 3), pp.3 -25.

 

Goman, M.G. & Khramtsovsky, A.V. (1990) Calculation of asymptotic stability region boundary of dynamic system. Uch. Zap. TsAGI, 21, (3), pp.59-68.

 

Goman, M.G., Stolyarov, G.I., Tyrtyshnikov, S.L., Usoltsev, S.P. & Khrabrov, A.N. (1990) Mathematical Description of Aircraft Longitudinal Aerodynamic Characteristics at High Angles of Attack Accounting for Dynamic Effects of Separated Flow. Preprint TsAGI No.9, pp. 38.

 

Goman, M.G., Klumov, A.S. & Merkulov, A.E. (1987) Compensation of inertia and kinematic coupling of longitudinal and lateral aircraft motions by means of automatic control. Proceeedings of TsAGI, Issue No. 2349, 43pp.

 

Goman, M.G., Zadoroznii, A.I. & Khrabrov, A.N. (1988) Asymmetrical vortex breakdown and aerodynamic hysteresis around a slender wing with conical body. Uch. Zap. TsAGI, 19, (1), pp. 1-7.

 

Goman, M.G., Milash, E.V. & Khramtsovsky, A.V. (1986) Interactive package for nonlinear aircraft dynamics investigation KRIT. Applied software for an aircraft aeromechanics problems, Issue 4, TsAGI.

 

Goman, M.G. & Khramtsovsky, A.V. (1986) Bifurcations of an aircraft spin regimes. Investigations in flight dynamics of flying vehicles, MIPhT, pp.17-25.

 

Goman, M. G., Zaharov, S.B. & Khrabrov, A.N. (1986) Bifurcatioins of vortical flow around slender wing with conical body. Proceedings of TsAGI, Issue No 2317, pp.42.

 

Goman, M. G. (1986) Differential method of continuation for system of nonlinear equations depending on a parameter. Uch. Zap. TsAGI, 17,(5), pp.42-51.

 

Goman, M. G., Zaharov, S.B. & Khrabrov, A.N. (1985) Aerodynamic hysteresis of vortical flow around a slender body. Dokl. Acad. Nauk SSSR, 282, (1).

 

Goman, M. G., Zaharov, S.B. & Khrabrov, A.N. (1985) Symmetrical and asymmetrical solutions in vortical ow problem for high sweep wing with conical body. Uch. Zap. TsAGI, 16, (5), 42-51.

 

Goman, M. G. & Khrabrov, A.N. (1985) Asymmetrical solutions in a vortical flow problem for plate with two sink-vortices. Izv. Akad. Nauk SSSR, Mech. Zhidk. & Gaza, part 3, pp. 42-48.

 

Goman, M. G. & Soukhanov, V.L. (1985) Self-oscillatory regimes of an aircraft rolling motion. Uch. Zap.TsAGI, 16, (2).

 

Goman, M. G. & Khrabrov, A.N. (1984) Calculation of asymmetrical vortical flow around slender body. Uch. Zap. TsAGI, 15 (6).

 

Goman M. G. (1983) Mathematical description of aerodynamic forces and moments at regimes with non-unique flow structure. Proceedings of TsAGI Issue No 2195, 49pp.

 

Goman, M. G. & Soukhanov, V.L. (1979) Calculation of longitudinal and lateral motion interaction during fast roll maneuvers. Manual for aircraft designers Vol 1 (Book 6), Issue 4, TsAGI, 82pp.

 

Goman, M. G. (1976) Unsteady resonance regimes of rotating vehicles with microasymmetry during re-entry in atmosphere. Uch. zap. TsAGI 7 (4), pp. 45-51.

 

Goman, M. G. (1975) Resonance regimes of rotating vehicles with plane of symmetry during re-entry in atmosphere. Proceedings of TsAGI Issue No.1714, 58pp.

 

Goman, M. G. & Shilov, A. A. (1974) Resonance regimes of axisymmetrical rotating vehicles during re-entry in atmosphere. Proceedings of TsAGI, Issue No.1649, 42pp.

 

 

Refereed Conference Publications:

 

M.Goman, & A.Khramtsovsky. Analysis of Aircraft Dynamcs Based on Parametric Continuation and Phase Portrait Investigation", 6th International Conference on Mathematical

Problems in Engineering and Aerospace Sciences, Budapest, Hungary, June 2006.

 

M.Goman, E.Kolesnikov, & A.Khramtsovsky. Computation of Attainable Equilibrium Sets for Analysis of Aircraft Performance and Manoeuvrability Characteristics", 6th International

Conference on Mathematical Problems in Engineering and Aerospace Sciences, Budapest, Hungary, June 2006.

 

M.Goman, M.Sidoryuk, & A.Ustinov. Control Law Design for Flexible Aircraft: Comparison of the H-infinity-based and Classical Methods", AIAA Guidance, Navigation, and Control

Conf. and Exhibit. AIAA Paper 2005-6265, San Francisco, CA, 2005.

 

N.Abramov, M.Goman,& A.Khrabrov. Lateral-Directional Aircraft Dynamics at High Incidence Flight with Account of Unsteady Aerodynamic Effects ", AIAA Atmospheric

Flight Mechanics Conf. and Exhibit. AIAA Paper 2005-6331, San Francisco, CA, 2005.

N.B.Abramov, M.G.Goman,& A.N.Khrabrov. Aircraft Dynamics at High Incidence Flight with Account of Unsteady Aerodynamic Effects ", AIAA Atmospheric Flight Mechanics

Conf. and Exhibit. AIAA Paper 2004-5274, Providence, RI, 2004.

 

M.G.Goman, Y.Patel & M.V.Sidoruck. Regions of Attraction for Robustness Assessment, AIAA Guidance, Navigation, and Control Conf. and Exhibit. AIAA Paper 2003-

5551, Austin, TX, 2003.

 

M.G.Goman, Y.Patel & A.V.Khramtsovsky. Flight Clearance Tools Using a Non-linear Bifurcation Analysis Framework", AIAA Guidance, Navigation, and Control Conf. and

Exhibit. AIAA Paper 2003-5557, Austin, TX, 2003.

 

M.G.Goman & M.N.Demenkov. Controllability Region Analysis for Unstable Aircraft Dynamics", AIAA Guidance, Navigation, and Control Conf. AIAA Paper 2002-4749,

Monterey, CA, 2002.

 

M.G.Goman & A.V.Khramtsovsky. Aerodynamics Modelling and Dynamics Simulation at High Angles of Attack", Inter. Conf. Simulation Technology & Training: Research,

Engineering & Martket Challenges, Zhukovsky, Russia, May 2001

 

M.G.Goman, D.I.Greenwell & A.N.Khrabrov. The Characteristic Time Constant Approach for Mathematical Modelling of High Angles of Attack Aerodynamics", The 22nd

ICAS Congress, Harrogate, UK, 2000.

 

N.B.Abramov, M.G.Goman, A.N.Khrabrov & D.I.Greenwell. Two-Step Linear Regression Method for Identification of High Incidence Unsteady Aerodynamic Model", AIAA

Atmospheric Flight Mechanics Conf. AIAA Paper 2001-4080, Montreal, Canada, 1999.

 

N.B.Abramov, M.G.Goman, A.N.Khrabrov & K.A.Kolinko. Simple Wings Unsteady Aerodynamics at High Angles of Attack: Experimental and Modeling Results", AIAA

Atmospheric Flight Mechanics Conf. AIAA Paper 99-4013, Portland, 1999.

 

D.I.Greenwell & M.G.Goman. Wind Tunnel Simulation of Combat Aircraft Manoeuvres, ICAS Paper, Melbourne, Australia, September 1998.

 

M.G.Goman & E.N.Kolesnikov. Robust Nonlinear Dynamic Inversion Method for an Aircraft Motion Control", AIAA Guidance, Navigation, and Control Conf. AIAA Paper

98-4208, 1998.

 

M.G.Goman & A.V.Khramtsovsky. Global Stability Analysis of Nonlinear Aircraft Dynamics, AIAA Guidance, Navigation, and Control Conf. AIAA Paper 97-3721, 1997.

 

M.G.Goman & E.V.Fedulova. Aircraft Dynamics Analysis and Control Law Design Taking Into Account Actuator Constraints", 4th Russian-Cino Conf. on Aerodynamics and Flight

Dynamics, Zhukovsky, Russia, May 1997.

 

M.G.Goman & E.N.Kolesnikov. Robust Control Law Design for an Aircraft Spatial Motion, Int. Symp. "Aviation 2000", Zhukovsky, Aug. 1997.

 

M.G.Goman, A.N.Khrabrov & S.P.Usoltsev. Unsteady Aerodynamic Model for Large Amplitude Maneuvers and Its Parameter Identification", 11th IFAC Symposium on System

Identification (SYSID'97), Japan, 1997.

 

M.G.Goman, A.V.Khramtsovsky & E.V.Fedulova. Maximum Stability Region Design for Unstable Aircraft with Control Constraints", AIAA Guidance, Navigation, and Control

Conf. AIAA Paper 96-3910, San Diego, CA, 1996.

 

M.G.Goman E.N.Kolesnikov. Aircraft motion control taking into account high level aerodynamic characteristics uncertainty", 4th Int. Workshop Stability and Oscillations of

Nonlinear Controllable Systems, Moscow, Russia, June 1996.

 

M.G.Goman & A.V.Khramtsovsky. Direct computational methods for regions of attraction of nonlinear dynamical system", 4th Int. Workshop Stability and Oscillations of Nonlinear

Controllable Systems, Moscow, Russia, June 1996.

 

M.G.Goman, E.N.Kolesnikov & F.Yu.Levada. Robust Control Law Design for an Aircraft Longitudinal Motion", Int. Symp. Experimental Facilities and Aircraft Certification,

Zhukovsky, Russia, Aug. 1995.

 

M.G.Goman, A.N.Khrabrov & S.P.Usoltsev. Identification of Unsteady Aerodynamic Model of a Delta Wing at High Angles of Attack", 10th IFAC Symposium on System

Identification (SYSID'94), Vol.3, pp.77-81, Copenhagen, Denmark, 1994.

 

M.G.Goman, A.V.Khramtsovsky, V.L.Soukhanov & V.A.Syrovatsky. Aircraft Spin Prevention/Recovery Control System", 3rd Russian-Cino Conference on Aerodynamics and

Flight Dynamics of Aircraft, Zhukovsky, Russia, Nov.1993.

 

M.G.Goman, E.V.Fedulova & A.V.Khramtsovsky. Maximum stability region for unstable aircraft with control constraints", Int. Conference on Flight Safety, TsAGI-AGARD

NATO, Zhukovsky, Russia, 1993.

 

M.G.Goman, A.N.Khrabrov & A.R.Studnev. Stochastic Self-Induced Oscillations of a Slender Delta Wing at High Angles of Attack", AIAA Atmospheric Flight Mechanics Conf.

AIAA Paper 92-4498, 1992.

 

M.G.Goman & A.N.Khrabrov. State-Space Representation of Aerodynamic Characteristics of an Aircraft at High Angles of Attack", AIAA Atmospheric Flight Mechanics Conf.

AIAA Paper 92-4651, 1992.

 

M.G.Goman, K.A.Kolinko, A.N.Khrabrov & S.P.Usoltsev. Investigation of Dynamics of Movable Aircraft Model on a Pendulum Support in Wind Tunnel", Int. Conf. Fundamental

Research in Aerospace Science, TsAGI, Moscow, 1992.

 

M.G. Goman & A.N.Khrabrov. Representation of aerodynamic characteristics at high angles of attack with account of dynamic effects of separated flow", 5th USSR Workshop

Modern problems in mechanics of fluid and gases , Irkutsk, 1990, pp.116-117.

 

M.G.Goman, S.B.Zaharov & A.N.Khrabrov. Asymmetrical critical structures and aerodynamic hysteresis in flow around a slender body, 4th USSR Workshop Modern problems

in mechanics of fluids and gases, Groznyi, 1986, pp.98-101.

 

M.G.Goman & A.V.Khramtsovsky. Qualitative investigation of nonlinear problems of an aircraft spatial motion", 6th USSR Congress on Theoretical and Applied Mechanics,

Tashkent, 1986.

M.G.Goman, A.S.Klumov, A.E.Merkulov & A.V.Khramtsovsky. Analysis of nonlinear aircraft dynamics and control law design for motion decoupling ", 5th USSR Conference

on Control in Mechanical Systems, Kazan, 1985.

 

G.I.Zagaynov & M.G.Goman. Bifurcation analysis of critical aircraft flight regimes, ICAS Paper, Vol 1, pp.217-223, Rome, 1984.

 

M.G.Goman & V.L.Soukhanov. About stability of an aircraft spatial motion", 5th USSR Congress on Theoretical and Applied Mechanics, Alma-Ata, 1981.