Orbit determination and differential-drag control of Planet Labs CubeSat constellations

C Foster, H Hallam, J Mason - arXiv preprint arXiv:1509.03270, 2015 - arxiv.org
We present methodology and mission results from orbit determination of Planet Labs
nanosatellites and differential-drag control of their relative motion. Orbit determination (OD) …

Constellation phasing with differential drag on planet labs satellites

C Foster, J Mason, V Vittaldev, L Leung… - Journal of Spacecraft …, 2018 - arc.aiaa.org
A methodology is presented for the differential drag control of a large fleet of propulsionless
satellites deployed in the same orbit. The controller places satellites into a constellation with …

Differential drag control scheme for large constellation of planet satellites and on-orbit results

C Foster, J Mason, V Vittaldev, L Leung… - arXiv preprint arXiv …, 2018 - arxiv.org
A methodology is presented for the differential drag control of a large fleet of propulsion-less
satellites deployed in the same orbit. The controller places satellites into a constellation with …

Attitude trajectory optimization for agile satellites in autonomous remote sensing constellations

E Sin, M Arcak, S Nag, V Ravindra, A Li… - AIAA Scitech 2021 …, 2021 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2021-1470. vid To maximize the utility of
remote sensing satellite constellations, agile attitude maneuvering is required. By taking into …

[HTML][HTML] Investigation of different strategies for access to space of small satellites on a defined LEO orbit

F Barato, E Toson, F Milza, D Pavarin - Acta Astronautica, 2024 - Elsevier
In recent years small satellites have shifted from being secondary items to dominate the
space market thanks to, but not only, the development of the large LEO constellations. For …

An integrated design methodology for the deployment of constellations of small satellites

NH Crisp, KL Smith, PM Hollingsworth - The Aeronautical Journal, 2019 - cambridge.org
A growing interest in constellations of small satellites has recently emerged due to the
increasing capability of these platforms and their reduced time and cost of development …

Small satellite constellation separation using linear programming based differential drag commands

E Sin, M Arcak, A Packard - 2018 Annual American Control …, 2018 - ieeexplore.ieee.org
We study the optimal control of an arbitrarily large constellation of small satellites operating
in low Earth orbit. Simulating the lack of on-board propulsion, we limit our actuation to the …

[PDF][PDF] A comprehensive examination of low earth orbit aerodynamic accelerations for satellite formation control

B Smith - 2019 - unsworks.unsw.edu.au
From satellite navigation to weather forecasting, the use of space technology is an
increasingly fruitful part of our everyday lives. A growing contingent of commercial …

Ground track control using differential drag for small earth observation satellite constellations

J Lee, H Bang - Journal of Spacecraft and Rockets, 2022 - arc.aiaa.org
This paper presents a framework for the acquisition and the maintenance of ground track
configurations of small Earth observation satellite constellations. Specifically, the relative …

Nanosatellite aerobrake maneuvering device

V Melnikova, A Borovikov, M Koretskii… - arXiv preprint arXiv …, 2017 - arxiv.org
In this paper, we present the project of the heliogyro solar sail unit for deployment of
CubeSat constellation and satellite deorbiting. The ballistic calculations show that …