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Anna
D.
Guerman
anna@ubi.pt
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Journal articles
2011
A A Burov
,
O I Kononov
,
A D Guerman
(2011)
Relative
equilibria
of
a
Moon
-
tethered
spacecraft
Advances in the Astronautical Sciences
136:
2553-2562
Abstract:
Notes:
DOI
R Gama
,
A Guerman
,
G Smirnov
(2011)
On
the
asymptotic
stability
of
discontinuous
systems
via
averaging
method.
Nonlinear Analysis Series A: Theory, Methods & Applications
74:
4.
1513–1522
Abstract:
Notes:
DOI
A D Guerman
,
A M V Seabra
,
G Smirnov
(2011)
Optimization
of
parameters
of
asymptotically
stable
systems.
Mathematical Problems in Engineering
Article ID 526167:
19 pp.
Abstract:
Notes:
A A Burov
,
A D Guerman
,
R S Sulikashvili
(2011)
On
steady-state
motions
of
gyrostats
with
equal
moments
of
inertia
in
a
central
force
field.
PMM – Journal of Applied Mathematics and Mechanics
75:
5.
739-745
Abstract:
Notes:
2010
DOI
A A Burov
,
A D Guerman
,
R S Sulikashvili
(2010)
The
orbital
motion
of
a
tetrahedral
gyrostat.
PMM – Journal of Applied Mathematics and Mechanics.
74:
4.
425-435.
Abstract:
Notes:
2009
DOI
A D Guerman
,
G Smirnov
,
M C Pereira
(2009)
Orbital
dynamics
of
a
Simple
Solar
Photon
Thruster
Mathematical Problems in Engineering
2009:
Article ID 537256
Abstract:
Notes:
2008
A D Guerman
,
G Smirnov
,
M C Pereira
(2008)
Attitude
dynamics
and
control
of
a
compound
solar
sail.
Advances in the Astronautical Sciences
129:
607-619
Abstract:
Notes:
DOI
V A Sarychev
,
P Paglione
,
A D Guerman
(2008)
Stability
of
equilibria
for
a
satellite
subject
to
gravitational
and
constant
torques.
Journal of Guidance, Control and Dynamics
31:
2.
386-394
Abstract:
Notes:
A A Burov
,
A D Guerman
,
R S Sulikashvili
(2008)
Relative
equilibria
of
a
tetrahedral
structure
with
rigid
and
tethered
elements.
Advances in the Astronautical Sciences
129:
1665-1674
Abstract:
Notes:
DOI
A D Guerman
,
G V Smirnov
,
P Paglione
,
A M Seabra
(2008)
Stationary
configurations
of
tetrahedral
tethered
satellite
formation.
Journal of Guidance, Control and Dynamics
31:
2.
424-428
Abstract:
Notes:
2007
DOI
A D Guerman
,
G Smirnov
(2007)
Comment
on
“Compound
Solar
Sail
with
Optical
Properties:
Models
and
Performance”.
Journal of Spacecraft and Rockets
44:
3.
732-734
Abstract:
Notes:
DOI
G V Smirnov
,
M Ovchinnikov
,
A Guerman
(2007)
Use
of
solar
radiation
pressure
to
maintain
a
spatial
satellite
formation.
Acta Astronautica
61:
7-8.
724-728
Abstract:
Notes:
DOI
M Yu Ovchinnikov
,
V D Shargorodsky
,
V I Pen'kov
,
S A Mirer
,
A D Guerman
,
R B Nemuchinsky
(2007)
Nanosatellite
REFLECTOR:
choice
of
parameters
of
the
attitude
control
system.
Cosmic Research
45:
60-77
Abstract:
Notes:
2006
M Yu Ovchinnikov
,
V D Shargorodsky
,
V I Pen'kov
,
S A Mirer
,
A D Guerman
(2006)
Passive
Attitude
Control
System
for
Nano-Satellite
REFLECTOR.
Advances in the Astronautical Sciences
123:
1217-1234
Abstract:
Notes:
DOI
A D Guerman
(2006)
Spatial
equilibria
of
multibody
chain
in
a
circular
orbit.
Acta Astronautica
58:
1.
1-14
Abstract:
Notes:
A Guerman
,
G Smirnov
(2006)
Attitude
Control
of
Solar
Photon
Thrustor
vs
Plane
Solar
Sail.
Advances in the Astronautical Sciences
123:
2635 - 2648
Abstract:
Notes:
2004
A D Guerman
,
S A Mirer
(2004)
Stationary
rotations
of
two
connected
axisymmetric
rigid
bodies.
Russian-American Journal on Actual Problems of Aviation and Aerospace Systems: Processes, Models, Experiments
9:
1(17).
60-76
Abstract:
Notes:
S A Agafonov
,
A D Guerman
(2004)
Stabilization
of
stationary
motion
of
gyrostat
satellite
by
means
of
external
moments.
Mechanics of Solids
39:
4.
3-6
Abstract:
Notes:
2003
DOI
A D Guerman
(2003)
Equilibria
of
multibody
chain
in
orbit
plane.
Journal of Guidance, Control and Dynamics
26:
6.
942-948
Abstract:
Notes:
DOI
V A Sarychev
,
A Guerman
,
P Paglione
(2003)
The
Influence
of
Constant
Torque
on
Equilibria
of
Satellite
in
Circular
Orbit.
Celestial Mechanics and Dynamical Astronomy.
87:
3.
219-239
Abstract:
Notes:
2002
A D Guerman
(2002)
Spatial
equilibria
of
an
n-link
chain
in
a
circular
orbit.
AIAA Meeting Papers on Disc
7:
4.
Abstract:
Notes:
A D Guerman
(2002)
Equilibria
of
an
n-link
chain
in
a
circular
orbit.
Advances in the Astronautical Sciences
112:
833-842
Abstract:
Notes:
2001
V A Sarychev
,
P Paglione
,
A Guerman
(2001)
Equilibria
of
a
satellite
subjected
to
a
constant
torque:
analysis
of
stability.
Advances in the Astronautical Sciences
108:
555-571
Abstract:
Notes:
1989
A D Guerman
,
M Yu Ovchinnikov
,
V I Pen´kov
,
V A Sarychev
(1989)
Non-resonant
motions
of
a
satellite
with
hysteresis
rods
under
conditions
of
gravity
orientation.
Mechanics of Solids
24:
6.
1-11
Abstract:
Notes:
V A Sarychev
,
V I Pen´kov
,
M Yu Ovchinnikov
,
A D Guerman
(1989)
Influence
of
a
hysteresis
rod
mounted
along
the
axis
of
maximum
moment
of
inertia
on
the
motion
of
a
satellite
in
the
gravity-oriented
attitude
control
mode.
Cosmic Research
27:
6.
727-737
Abstract:
Notes:
1988
V A Sarychev
,
M Yu Ovchinnikov
,
A D Guerman
(1988)
Periodic
motions
of
a
satellite
with
a
strong
magnet
in
the
plane
of
a
polar
orbit.
Cosmic Research
26:
6.
830 - 839
Abstract:
Notes:
V A Sarychev
,
V I Pen´kov
,
M Yu Ovchinnikov
,
A D Guerman
(1988)
Motions
of
a
gravitationally
stabilized
satellite
with
hysteresis
rods
in
a
polar
orbit.
Cosmic Research
26:
5.
561-574
Abstract:
Notes:
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