A review of space-object collision probability computation methods
The collision probability computation of space objects plays an important role in space
situational awareness, particularly for conjunction assessment and collision avoidance …
situational awareness, particularly for conjunction assessment and collision avoidance …
Low-thrust reconfiguration strategy and optimization for formation flying using Jordan normal form
X Bai, Y He, M Xu - IEEE Transactions on Aerospace and …, 2021 - ieeexplore.ieee.org
This article proposes a low-thrust reconfiguration strategy for formation flying based on the
Jordan normal form and evaluates its performance based on the required control …
Jordan normal form and evaluates its performance based on the required control …
A survey of underwater docking guidance systems
Autonomous underwater vehicles (AUVs) are increasingly being used for underwater survey
and exploration missions. The expanding mission scope for AUVs highlights the need for a …
and exploration missions. The expanding mission scope for AUVs highlights the need for a …
An optimal control-based path planning method for unmanned surface vehicles in complex environments
This paper proposes an optimal control-based method named the rapid-Gauss
pseudospectral method (RGPM) to obtain a smooth time-optimal path for unmanned surface …
pseudospectral method (RGPM) to obtain a smooth time-optimal path for unmanned surface …
Distributed game strategy for formation flying of multiple spacecraft with disturbance rejection
J Li, S Chen, C Li, F Wang - IEEE Transactions on Aerospace …, 2020 - ieeexplore.ieee.org
This article investigates a distributed game strategy for formation control of multispacecraft
subjected to nonlinear dynamics and J 2 perturbations. In the proposed problem, each …
subjected to nonlinear dynamics and J 2 perturbations. In the proposed problem, each …
Model predictive control switching strategy for safe small satellite cluster formation flight
T Smith, J Akagi, G Droge - Aerospace Systems, 2023 - Springer
This paper presents the development and analysis of a spacecraft formation flying
architecture. The desired state of each spacecraft is maintained using a model predictive …
architecture. The desired state of each spacecraft is maintained using a model predictive …
Fuel optimization for continuous-thrust orbital rendezvous with collision avoidance constraint
R Epenoy - Journal of Guidance, Control, and Dynamics, 2011 - arc.aiaa.org
This paper focuses on the issue of minimum-fuel rendezvous between an active chaser
satellite with continuousthrust capability and a passive target satellite. It is first formalized as …
satellite with continuousthrust capability and a passive target satellite. It is first formalized as …
Rapid cooperative optimization of continuous trajectory for electric sails in multiple formation reconstruction scenarios
R **, M Huo, Y Xu, C Zhao, L Yang, N Qi - Aerospace Science and …, 2023 - Elsevier
In satellite formation missions, conventional low-thrust spacecraft need to continuously
consume fuel to maintain a stable formation configuration, which limits the mission period …
consume fuel to maintain a stable formation configuration, which limits the mission period …
Shape-based analytic safe trajectory design for spacecraft equipped with low-thrust engines
K Zeng, Y Geng, B Wu - Aerospace Science and Technology, 2017 - Elsevier
To rapidly design three dimensional low-thrust safe trajectories for spacecraft orbit transfer
and rendezvous problems, an analytic shape-based approach is proposed. Unlike some …
and rendezvous problems, an analytic shape-based approach is proposed. Unlike some …
Fast costate estimation for indirect trajectory optimization using Bezier-curve-based sha** approach
M Huo, L Yang, N Peng, C Zhao, W Feng, Z Yu… - Aerospace Science and …, 2022 - Elsevier
In this study, a fast costate estimation method derived from the Bezier-curve-based sha**
approach is proposed for indirect low-thrust transfer trajectory optimization. The trajectory is …
approach is proposed for indirect low-thrust transfer trajectory optimization. The trajectory is …