peer reviewedAutonomous formation flight enables new satellite missions for novel applications. The cost and limits of propulsion systems can be overcome if environmental resources are being benefitted of. Currently, atmospheric drag is used in low Earth orbit to this end. Solar radiation pressure, which is of similar order of magnitude as aerodynamic ram pressure, is, however, always neglected. We introduce this force and show that it can be exploited. We demonstrate through simulations that a formation geometry is established quicker if the solar radiation pressure is modeled
A real alternative to Lagrange point very low perturbed orbits, for universe observation missions, i...
In recent years, thanks to advancements in commercial hardware technology miniaturization, small sat...
A deorbiting strategy for small satellites, in particular CubeSats, is proposed which exploits the e...
peer reviewedAutonomous formation flight enables new satellite missions for novel applications. The ...
Using several small, unconnected satellites flying in formation rather than a single monolithic sate...
As the SSA system upgrades its existing capabilities and adds new ones, the potential offered by ine...
Nanosats are a new class of low mass satellite amenable to solar pressure propulsion. Carnegie Mello...
For a satellite formation to maintain its intended design despite present perturbations (formation k...
This paper discusses the use of solar radiation pressure (SRP) augmented deorbiting to passively rem...
The mass, volume and launch constraints of CubeSats has resulted in operators resorting to the drag ...
This paper investigates how the perturbations due to asymmetric solar radiation pressure, in presenc...
Due to mass and volume constraints on planetary missions, the development of control techniques that...
The effect of solar radiation pressure and atmospheric drag on the orbital dynamics of satellites-on...
The effect of solar radiation pressure and atmospheric drag on the orbital dynamics of satellites-on...
This study investigates the use of a linear quadratic terminal controller to reconfigure satellite f...
A real alternative to Lagrange point very low perturbed orbits, for universe observation missions, i...
In recent years, thanks to advancements in commercial hardware technology miniaturization, small sat...
A deorbiting strategy for small satellites, in particular CubeSats, is proposed which exploits the e...
peer reviewedAutonomous formation flight enables new satellite missions for novel applications. The ...
Using several small, unconnected satellites flying in formation rather than a single monolithic sate...
As the SSA system upgrades its existing capabilities and adds new ones, the potential offered by ine...
Nanosats are a new class of low mass satellite amenable to solar pressure propulsion. Carnegie Mello...
For a satellite formation to maintain its intended design despite present perturbations (formation k...
This paper discusses the use of solar radiation pressure (SRP) augmented deorbiting to passively rem...
The mass, volume and launch constraints of CubeSats has resulted in operators resorting to the drag ...
This paper investigates how the perturbations due to asymmetric solar radiation pressure, in presenc...
Due to mass and volume constraints on planetary missions, the development of control techniques that...
The effect of solar radiation pressure and atmospheric drag on the orbital dynamics of satellites-on...
The effect of solar radiation pressure and atmospheric drag on the orbital dynamics of satellites-on...
This study investigates the use of a linear quadratic terminal controller to reconfigure satellite f...
A real alternative to Lagrange point very low perturbed orbits, for universe observation missions, i...
In recent years, thanks to advancements in commercial hardware technology miniaturization, small sat...
A deorbiting strategy for small satellites, in particular CubeSats, is proposed which exploits the e...