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Multi-Agent Spacecraft Attitude Formation and Tracking Control Using Reshaping
by
Butcher, Eric A.
, Mathavaraj, S.
in
Aerospace Technology and Astronautics
/ Communication
/ Control algorithms
/ Engineering
/ Equilibrium
/ Kinematics
/ Liapunov functions
/ Lie groups
/ Mathematical Applications in the Physical Sciences
/ Multiagent systems
/ Original Article
/ Simulation
/ Space Exploration and Astronautics
/ Space Sciences (including Extraterrestrial Physics
/ Spacecraft
/ Spacecraft attitude control
/ Spacecraft tracking
/ Synchronism
/ Topology
/ Tracking control
2025
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Multi-Agent Spacecraft Attitude Formation and Tracking Control Using Reshaping
by
Butcher, Eric A.
, Mathavaraj, S.
in
Aerospace Technology and Astronautics
/ Communication
/ Control algorithms
/ Engineering
/ Equilibrium
/ Kinematics
/ Liapunov functions
/ Lie groups
/ Mathematical Applications in the Physical Sciences
/ Multiagent systems
/ Original Article
/ Simulation
/ Space Exploration and Astronautics
/ Space Sciences (including Extraterrestrial Physics
/ Spacecraft
/ Spacecraft attitude control
/ Spacecraft tracking
/ Synchronism
/ Topology
/ Tracking control
2025
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Do you wish to request the book?
Multi-Agent Spacecraft Attitude Formation and Tracking Control Using Reshaping
by
Butcher, Eric A.
, Mathavaraj, S.
in
Aerospace Technology and Astronautics
/ Communication
/ Control algorithms
/ Engineering
/ Equilibrium
/ Kinematics
/ Liapunov functions
/ Lie groups
/ Mathematical Applications in the Physical Sciences
/ Multiagent systems
/ Original Article
/ Simulation
/ Space Exploration and Astronautics
/ Space Sciences (including Extraterrestrial Physics
/ Spacecraft
/ Spacecraft attitude control
/ Spacecraft tracking
/ Synchronism
/ Topology
/ Tracking control
2025
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Multi-Agent Spacecraft Attitude Formation and Tracking Control Using Reshaping
Journal Article
Multi-Agent Spacecraft Attitude Formation and Tracking Control Using Reshaping
2025
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Overview
In this paper the problems of multi-agent spacecraft attitude formation and tracking control on
T
S
O
(
3
)
N
are addressed using rotation matrices and globally continuous control protocols derived using Morse-Bott-Lyapunov functions, including a feedback reshaping strategy for enlarging the region of attraction of the desired equilibrium manifold. For attitude formation control the spacecraft comes to rest with desired relative attitudes between connected pairs according to the specified communication topology. Examples include
N
spacecraft with undirected ring or complete graph topologies achieving a desired balanced configuration on the circle or on
SO
(3). The proposed attitude formation tracking control protocol, which extends a proposed tracking controller for a single spacecraft on
TSO
(3), consists of one or more leaders tracking a time-varying command while the followers either achieve attitude synchronization or a desired time-varying attitude formation with the leaders.
Publisher
Springer US,Springer Nature B.V
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