[PDF][PDF] Satellite re-entry modeling and uncertainty quantification

M Horsley - 2012 - osti.gov
ABSTRACT LEO trajectory modeling is a fundamental aerospace capability and has
applications in many areas of aerospace, such as maneuver planning, sensor scheduling, re …

Detailed analysis of aerodynamic effect on small satellites

K Miyata, R Kawashima, T Inamori - TRANSACTIONS OF THE …, 2018 - jstage.jst.go.jp
A company report1) forecasts a growth in the number of the planning small satellite projects
despite the shortage of launch opportunities. Low Earth Orbit (LEO) is one of the most …

[引用][C] Impact of non-gravitational forces on GPS-based precise orbit determination of low Earth orbiters

VEJ Girardin - 2016

A review and gap analysis of exploiting aerodynamic forces as a means to control satellite formation flight

C Traub, F Romano, T Binder… - Deutscher Luft-und …, 2018 - upcommons.upc.edu
Using several small, unconnected satellites flying in formation rather than a single
monolithic satellite has many advantages. As an example, separate optical systems can be …

Measuring absolute thermospheric densities and accommodation coefficients using paddlewheel satellites: past findings, present uses, and future mission concepts

MD Pilinski, K Moe, SE Palo, BM Argrow - The Journal of the Astronautical …, 2011 - Springer
The first absolute measurement of thermospheric density was made by combining
simultaneous observations of spin and semimajor axis decay of Explorer VI. Providing two …

Aerodynamic attitude control of ultra-low earth orbit satellite

L Chen, H Gui, S Xiao - … Conference on Guidance, Navigation and Control, 2022 - Springer
This paper describes a method for active attitude control using only aerodynamic torque in
ultra-low orbit. A satellite with four panels is studied and the simplified method for calculating …

[PDF][PDF] The effect of different adsorption models on satellite drag coefficients

AC Walker, P Mehta, J Koller - Advances in the Astronautical …, 2013 - researchgate.net
Accurate satellite drag coefficients are important for reducing orbit prediction errors and for
inferring unbiased atmospheric mass density from measurements of satellite decay. Past …

[PDF][PDF] Progress in satellite formation flight control using differential aerodynamic forces made at the Institute of Space Systems (IRS)

C Traub, S Fasoulas, G Herdrich - AAS/AIAA Astrodynamics …, 2020 - researchgate.net
This paper gives a comprehensive summary of the progress in the field of satellite formation
flight control via differential aerodynamic forces made at the Institute of Space Systems of the …

[PDF][PDF] Rendezvous maneuvers of small spacecraft using differential lift and drag

M Horsley, S Nikolaev, A Pertica - 2011 - osti.gov
Rendezvous Maneuvers of Small Spacecraft Using Differential Lift and Drag Page 1 LLNL-JRNL-520611
Rendezvous Maneuvers of Small Spacecraft Using Differential Lift and Drag M. Horsley, S …

High-fidelity dynamic modeling of spacecraft in the continuum–rarefied transition regime

CP Turansky - 2012 - search.proquest.com
The state of the art of spacecraft rarefied aerodynamics seldom accounts for detailed rigid-
body dynamics. In part because of computational constraints, simpler models based upon …