This research addresses the high CubeSat mission failure rates caused by inadequate software and overreliance on ground control. By applying a reliable design methodology to flight software development and developing an onboard digital twin platform with fault prediction capabilities, this study provides a solution to increase satellite resilience and autonomy, thus reducing the risk of mission failure. These findings have implications for spacecraft of all sizes, paving the way for more resilient space missions
There are multiple common reasons for CubeSats’ failure. These include power, mechanical, and commun...
The Deployable Optical Receiver Aperture (DORA) CubeSat is a 3U CubeSat that seeks to demonstrate da...
In the last twenty years, CubeSat Systems have gained popularity in educational institutions and com...
Space missions force engineers to make complex trade-offs between many different constraints includi...
The utility of Small Satellites (SmallSats) for technology demonstrations and scientific research ha...
When space programs launch vehicles into orbit, multiple failures could arise throughout the mission...
The large-scale development and deployment of small satellite systems in the modern aerospace sector...
Much more than fault tolerance, space applications require dependability, which is the combination o...
Failure detection, identification and recovery (FDIR) has been an important and necessary instrume...
Today, more satellites are being launched at a rate never experienced before. This is due, in part, ...
This paper describes some important aspects of high- integrity software development based on the aut...
For many years, traditional satellite design philosophy was dominated by highly reliable components,...
Objectives Enabling Mission Success and effective design improvements Identify Risk (safety, perfo...
textRisk management plans improve the likelihood of mission success by identifying potential failure...
Miniaturized satellites enable a variety space missions which were in the past infeasible, impractic...
There are multiple common reasons for CubeSats’ failure. These include power, mechanical, and commun...
The Deployable Optical Receiver Aperture (DORA) CubeSat is a 3U CubeSat that seeks to demonstrate da...
In the last twenty years, CubeSat Systems have gained popularity in educational institutions and com...
Space missions force engineers to make complex trade-offs between many different constraints includi...
The utility of Small Satellites (SmallSats) for technology demonstrations and scientific research ha...
When space programs launch vehicles into orbit, multiple failures could arise throughout the mission...
The large-scale development and deployment of small satellite systems in the modern aerospace sector...
Much more than fault tolerance, space applications require dependability, which is the combination o...
Failure detection, identification and recovery (FDIR) has been an important and necessary instrume...
Today, more satellites are being launched at a rate never experienced before. This is due, in part, ...
This paper describes some important aspects of high- integrity software development based on the aut...
For many years, traditional satellite design philosophy was dominated by highly reliable components,...
Objectives Enabling Mission Success and effective design improvements Identify Risk (safety, perfo...
textRisk management plans improve the likelihood of mission success by identifying potential failure...
Miniaturized satellites enable a variety space missions which were in the past infeasible, impractic...
There are multiple common reasons for CubeSats’ failure. These include power, mechanical, and commun...
The Deployable Optical Receiver Aperture (DORA) CubeSat is a 3U CubeSat that seeks to demonstrate da...
In the last twenty years, CubeSat Systems have gained popularity in educational institutions and com...