Attitude dynamics of spacecraft with time-varying inertia during on-orbit refueling
Z Guang, Z Heming, B Liang - Journal of Guidance, Control, and …, 2018 - arc.aiaa.org
On-orbit refueling technologies provide a new way to extend the lifespan of satellites that run
out of propellant. During propellant transfer, the equivalent mass redistribution between the …
out of propellant. During propellant transfer, the equivalent mass redistribution between the …
Modeling and control for spacecraft relative pose motion by using twistor representation
Y Deng, Z Wang - Journal of Guidance, Control, and Dynamics, 2016 - arc.aiaa.org
THE coupling effect between spacecraft translational motion and rotational motion cannot be
ignored in advanced space missions, such as spacecraft formation flying, proximity …
ignored in advanced space missions, such as spacecraft formation flying, proximity …
A generalized control law for uniform, global and exponential magnetic detumbling of rigid spacecraft
The problem of magnetic detumbling, also known as magnetic momentum unloading, is
considered. The objective is to stabilize a rigid spacecraft angular velocity to zero only …
considered. The objective is to stabilize a rigid spacecraft angular velocity to zero only …
[PDF][PDF] I. Earned Degrees
P TSIOTRAS - dcsl.gatech.edu
Coordinated all campus activities in the area of autonomy. Administered the IRIM Seed
Grants program, established and administered the IRIM Visiting Faculty and Resident …
Grants program, established and administered the IRIM Visiting Faculty and Resident …