Using modern mathematic tool sets, various general perturbations methods such as the methods developed by the authors1,2, by Cook, King-Hele & Walker3 or by Griffin & French4 among others can be enhanced with the development of an average projected area model. A new method of determining the average projected area of a tumbling CubeSat is presented, which improves on the accuracy of the method recommended in Section 6.3 of the ISO standard 27852:2010(E)5. This enhancement can be applied to many different general perturbations methods and due to its simple mathematical nature it allows users to perform rapid Monte-Carlo analyses with thousands of permutations of the problem. Traditional numerical or even semi-analytical solutions would requi...
Once a satellite has completed its operational period, it must be removed responsibly in order to re...
Precision mean element (PME) satellite theories play a key role in orbit dynamics analyses. These th...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1993.In...
Using modern mathematic tool sets, various general perturbations methods such as the methods develop...
The general perturbations method for orbit lifetime analysis developed by the authors is improved by...
A new parameter is introduced, termed the density index, which enables the solar activity cycle to b...
A general perturbations method for orbit lifetime analysis is extended to include an analytical non-...
An analytical atmospheric density model, including solar activity effects, is applied to an analytic...
Geostationary orbit (GEO) is the most commercially valuable Earth orbit. The Inter-Agency Space Debr...
Satellite drag variability caused by the dynamics of the upper atmosphere is a major cause of orbit ...
Given the dynamic environment in which spacecraft exist, a better methodology for performing orbital...
High area-to-mass-ratio spacecraft experience a signifcant perturbation due to surface forces, such ...
Current analytical satellite vulnerability planning in the U.S. Space Surveillance System is reliant...
In the special perturbation method, Cowell and variation-of-parameters formulations of the motion eq...
Several methods are presented for the design of satellite formations for science missions in high-ec...
Once a satellite has completed its operational period, it must be removed responsibly in order to re...
Precision mean element (PME) satellite theories play a key role in orbit dynamics analyses. These th...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1993.In...
Using modern mathematic tool sets, various general perturbations methods such as the methods develop...
The general perturbations method for orbit lifetime analysis developed by the authors is improved by...
A new parameter is introduced, termed the density index, which enables the solar activity cycle to b...
A general perturbations method for orbit lifetime analysis is extended to include an analytical non-...
An analytical atmospheric density model, including solar activity effects, is applied to an analytic...
Geostationary orbit (GEO) is the most commercially valuable Earth orbit. The Inter-Agency Space Debr...
Satellite drag variability caused by the dynamics of the upper atmosphere is a major cause of orbit ...
Given the dynamic environment in which spacecraft exist, a better methodology for performing orbital...
High area-to-mass-ratio spacecraft experience a signifcant perturbation due to surface forces, such ...
Current analytical satellite vulnerability planning in the U.S. Space Surveillance System is reliant...
In the special perturbation method, Cowell and variation-of-parameters formulations of the motion eq...
Several methods are presented for the design of satellite formations for science missions in high-ec...
Once a satellite has completed its operational period, it must be removed responsibly in order to re...
Precision mean element (PME) satellite theories play a key role in orbit dynamics analyses. These th...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1993.In...