Scalable Satellite Swarm Deployment via Distance-based Orbital Transition Under $J_2$ Perturbation
Yuta Takahashi, Shin-ichiro Sakai

TL;DR
This paper introduces a decentralized, fuel-free guidance and control strategy for deploying satellite swarms into stable, coplanar formations in $J_2$-perturbed orbits, ensuring long-term stability and scalability.
Contribution
It develops a novel distance-based orbital stabilizer and deployment controller that operate autonomously without thrusters, addressing control loss risks during formation deployment.
Findings
Successful autonomous deployment into coplanar formations
Long-term stability achieved with fuel-free actuation methods
Robustness against communication outages demonstrated
Abstract
This paper presents an autonomous guidance and control strategy for a satellite swarm that enables scalable distributed space structures for innovative science and business opportunities. The averaged orbital parameters that describe the drift and periodic orbital motion were derived along with their target values to achieve a distributed space structure in a decentralized manner. This enabled the design of a distance-based orbital stabilizer to ensure autonomous deployment into a monolithic formation of a coplanar equidistant configuration on a user-defined orbital plane. Continuous formation control was assumed to be achieved through fuel-free actuation, such as satellite magnetic field interaction and differential aerodynamic forces, thereby maintaining long-term formation stability without thruster usage. A major challenge for such actuation systems is the potential loss of…
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Taxonomy
TopicsSpacecraft Dynamics and Control · Space Satellite Systems and Control · Satellite Communication Systems
