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Review of attitude consensus of multiple spacecraft
A group of cooperative agents can finish complicated missions that are difficult for a large
machine. In the past two decades, spacecraft attitude coordination has attracted significant …
machine. In the past two decades, spacecraft attitude coordination has attracted significant …
Rigid-body attitude control
NA Chaturvedi, AK Sanyal… - IEEE control systems …, 2011 - ieeexplore.ieee.org
Rigid-body attitude control is motivated by aerospace applications that involve attitude
maneuvers or attitude stabilization. The set of attitudes of a rigid body is the set of 3 X 3 …
maneuvers or attitude stabilization. The set of attitudes of a rigid body is the set of 3 X 3 …
Stability of a bottom-heavy underwater vehicle
NE Leonard - Automatica, 1997 - Elsevier
We study stability of underwater vehicle dynamics for a six-degree-of-freedom vehicle
modeled as a neutrally buoyant, submerged rigid body in an ideal fluid. We consider the …
modeled as a neutrally buoyant, submerged rigid body in an ideal fluid. We consider the …
Feedback control for spacecraft reorientation under attitude constraints via convex potentials
A novel guidance algorithm is proposed for the attitude reorientation of a rigid body
spacecraft in the presence of multiple types of attitude-constrained zones. In this direction …
spacecraft in the presence of multiple types of attitude-constrained zones. In this direction …
Control of underactuated spacecraft with bounded inputs
P Tsiotras, J Luo - Automatica, 2000 - Elsevier
We provide stabilizing feedback control laws for the kinematic system of an underactuated
axisymmetric spacecraft subject to input constraints. The proposed control law forces all …
axisymmetric spacecraft subject to input constraints. The proposed control law forces all …
Control of spacecraft subject to actuator failures: State-of-the-art and open problems
P Tsiotras, V Doumtchenko - The Journal of the Astronautical Sciences, 2000 - Springer
In this paper we review the main results in the area of active control of spacecraft with one
actuator failure. We emphasize the qualitative characteristics that make this a challenging …
actuator failure. We emphasize the qualitative characteristics that make this a challenging …
Backstep**-based steering control for spacecraft attitude control using two-skewed control moment gyroscopes
H Kojima - Journal of Guidance, Control, and Dynamics, 2023 - arc.aiaa.org
Numerous control methods that use two reaction wheels have been proposed for the
underactuated control problem. However, few studies have applied two single-gimbal …
underactuated control problem. However, few studies have applied two single-gimbal …
Control design for chained-form systems with bounded inputs
J Luo, P Tsiotras - Systems & control letters, 2000 - Elsevier
Discontinuous, time-invariant controllers have been recently proposed in the literature as an
alternative method to stabilize nonholonomic systems. These control laws are not …
alternative method to stabilize nonholonomic systems. These control laws are not …
Attitude control of an underactuated spacecraft using tube-based MPC approach
M Mirshams, M Khosrojerdi - Aerospace Science and Technology, 2016 - Elsevier
Feasibility of achieving 3-axis stabilization of an asymmetric spacecraft for cases where
there is no control available in one axis (underactuated spacecraft) is explored in this paper …
there is no control available in one axis (underactuated spacecraft) is explored in this paper …
Nonlinear attitude and shape control of spacecraft with articulated appendages and reaction wheels
C Rui, IV Kolmanovsky… - IEEE Transactions on …, 2000 - ieeexplore.ieee.org
Three-dimensional attitude and shape control problems are studied for a class of spacecraft
with articulated appendages and reaction wheels. A number of special cases of such …
with articulated appendages and reaction wheels. A number of special cases of such …