Approximate optimal LEO transfers with J2 perturbation and dragsail
L Casalino, A Forestieri - Acta Astronautica, 2022 - Elsevier
An indirect optimization method is applied to orbit transfers in LEO, considering almost
circular orbits and the influence of J2 perturbation. An approach based on Edelbaum's …
circular orbits and the influence of J2 perturbation. An approach based on Edelbaum's …
Deorbiting Perfomance of Electrodynamic Tethers to Mitigate Space Debris
G Sarego, L Olivieri, A Valmorbida… - … Journal of Aerospace …, 2021 - research.unipd.it
International guidelines recommend removing any artificial body in Low Earth Orbit (LEO)
within 25 years from mission completion. Among disposal strategies, electrodynamic tethers …
within 25 years from mission completion. Among disposal strategies, electrodynamic tethers …
Propelling the Future: Advanced Electric Propulsion Systems for Unmanned Aerial Vehicles
Due to their numerous uses in industries including surveillance, agriculture, mapping, and
delivery services, unmanned aerial vehicles (UAVs) have attracted a lot of attention in recent …
delivery services, unmanned aerial vehicles (UAVs) have attracted a lot of attention in recent …
Collision probability of composite cubesats hovering in leader-follower configuration
Y Xie, K Chan, J Zhang - Acta Astronautica, 2020 - Elsevier
Analytical expressions are obtained for computing the collision probability of a large
Composite CubeSats hovering in the close vicinity of another large Composite CubeSats in …
Composite CubeSats hovering in the close vicinity of another large Composite CubeSats in …
[HTML][HTML] Development of Drag Augmentation Device for Post Mission Disposal of Nanosatellite
JS Kim, HD Kim - Journal of Space Technology and Applications, 2022 - jstna.org
요약 본 논문에서는 초소형위성용 항력 증대 장치 개발에 대해 기술하였다. 최근 우주 개발이
New Space 시대에 접어들며, 소형 로켓 및 초소형위성 거대 군집 운용 등 인공물체의 저궤도 …
New Space 시대에 접어들며, 소형 로켓 및 초소형위성 거대 군집 운용 등 인공물체의 저궤도 …
[PDF][PDF] Establishment of Numerical Analysis Method and Orbit Demonstration of Membrane Structure Deployment Behavior using Self-extending Booms under …
AAAAP Pala - tohoku.repo.nii.ac.jp
Since the launch of the first artificial Earth satellite Sputnik 1 in 1957, mankind has been
launching various objects into space. Many of these objects, including once useful satellites …
launching various objects into space. Many of these objects, including once useful satellites …
[图书][B] Passive drag sail applications for the accelerated deorbit and targeted reentry of spacecraft
AM Sweeten - 2021 - search.proquest.com
In the relatively short time that space has been an asset to humans, the amount of debris
occupying the region has become a noticeable concern. Maintaining the usability of space …
occupying the region has become a noticeable concern. Maintaining the usability of space …
[PDF][PDF] 초소형위성의폐기기동을위한항력증대장치개발
김지석， 김해동 - 우주기술과응용, 2022 - researchgate.net
요 약본 논문에서는 초소형위성용 항력 증대 장치 개발에 대해 기술하였다. 최근 우주 개발이
New Space 시대에 접어들며, 소형 로켓 및 초소형위성 거대 군집 운용 등 인공물체의 저궤도 …
New Space 시대에 접어들며, 소형 로켓 및 초소형위성 거대 군집 운용 등 인공물체의 저궤도 …
Long-Term Sustainability of Space and Sustainability Requirements
D McKnight - Handbook of Small Satellites: Technology, Design …, 2020 - Springer
Small satellites must be designed and operated to support the long-term sustainability of
safe space operations. This community responsibility is reflected in the debris mitigation …
safe space operations. This community responsibility is reflected in the debris mitigation …