This paper studies the interaction between two satellites after docking. In order to maintain the docked state with uncertainty in the motion of the target vehicle, a game theoretic controller with Stackelberg strategy to minimize the interaction between the satellites is considered. The small perturbation approximation leads to LQ differential game scheme, which is validated to address the docking interactions between a service vehicle and a target vehicle. The open-loop solution are compared with Nash strategy, and it is shown that less control efforts are obtained with Stackelberg strategy
This thesis addresses several aerospace guidance and decision making problems using both no cooperat...
Industrial robots are often used for the simulation of satellites during on orbit servicing. In orde...
The implementation of a model-free, off-policy, actor-critic deep reinforcement learning algorithm c...
The rendezvous problem between two active spacecraft is formulated as a two player nonzero-sum diff...
This paper develops and evaluates a trust-based sensor management game-theoretical control approach ...
This work presents a non-linear control strategy for the docking of two spacecraft in a leader-follo...
We investigate trajectory generation algorithms that allow a satellite to autonomously rendezvous an...
Abstract: Capturing disused satellites in orbit and their controlled reentry is the aim of the DEOS ...
This paper presents a study on spacecraftRendezvous and Docking (RvD) through a comprehensiveliterat...
113 p.Thesis (Ph.D.)--University of Illinois at Urbana-Champaign, 1985.Optimal open loop and nonline...
Multi-body spacecraft attitude and configuration control formulations based on the use of collaborat...
Abstract. In this paper we present a study on the Collision-Avoidance mode of a formation flying sa...
Docking an in-orbit satellite by another satellite is a challenging task, especially when the target...
The spacecraft’s lifetime is often limited by reliability and redundancy of its components. Furtherm...
The paper proposes an algorithm for solving the optimal open-loop terminal control problem of two sp...
This thesis addresses several aerospace guidance and decision making problems using both no cooperat...
Industrial robots are often used for the simulation of satellites during on orbit servicing. In orde...
The implementation of a model-free, off-policy, actor-critic deep reinforcement learning algorithm c...
The rendezvous problem between two active spacecraft is formulated as a two player nonzero-sum diff...
This paper develops and evaluates a trust-based sensor management game-theoretical control approach ...
This work presents a non-linear control strategy for the docking of two spacecraft in a leader-follo...
We investigate trajectory generation algorithms that allow a satellite to autonomously rendezvous an...
Abstract: Capturing disused satellites in orbit and their controlled reentry is the aim of the DEOS ...
This paper presents a study on spacecraftRendezvous and Docking (RvD) through a comprehensiveliterat...
113 p.Thesis (Ph.D.)--University of Illinois at Urbana-Champaign, 1985.Optimal open loop and nonline...
Multi-body spacecraft attitude and configuration control formulations based on the use of collaborat...
Abstract. In this paper we present a study on the Collision-Avoidance mode of a formation flying sa...
Docking an in-orbit satellite by another satellite is a challenging task, especially when the target...
The spacecraft’s lifetime is often limited by reliability and redundancy of its components. Furtherm...
The paper proposes an algorithm for solving the optimal open-loop terminal control problem of two sp...
This thesis addresses several aerospace guidance and decision making problems using both no cooperat...
Industrial robots are often used for the simulation of satellites during on orbit servicing. In orde...
The implementation of a model-free, off-policy, actor-critic deep reinforcement learning algorithm c...