**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.

**(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,

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,

**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 *

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. & *

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*, **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*, **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, *

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, *

* *

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, *

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*, **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, *

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

**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*, **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*, **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*, **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*, **1999.**

D.I.Greenwell & M.G.Goman. Wind
Tunnel Simulation of Combat Aircraft Manoeuvres, *ICAS
Paper*, **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*, **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)*, **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*, **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*, **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*,

**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, **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*, **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*, **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,
**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 *

*Modern
problems in mechanics of fluid and gases ,* **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 *

*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 *,

**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 *

*on** Control in Mechanical Systems*, **1985**.

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

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