Add to ORKGObjectives: Modular ADCS based on CubeSat flight experience, space heritage hardware and rad hard components for small satellites Project goal: Integration of independent modules based on electronic data sheets (EDS) configuration system Capabilities: Attitude determination and control Boot and self-recovery Plug and play interface to sensor and actuators Fault Detection, Isolation & Recovery (FDIR) Data management and storage External control interfac
Since the beginning of space history new innovative ideas have been driving space scientists to deve...
Guidance, navigation, and control (GNC) systems are commonly found in vehicles, whether they be spac...
Spacecraft modularity is a powerful design methodology for shortening satellite development cycles a...
This thesis describes the development of the Attitude Determination and Control System (ADCS) for Cu...
In an attempt to reduce the cost of future satellites, new technologies are being pursued to develop...
The design and testing of AFIT\u27s 6U Attitude Determination and Control Subsystem (ADCS) are explo...
The design and testing of AFIT\u27s 6U Attitude Determination and Control Subsystem (ADCS) are explo...
The design and testing of AFIT\u27s 6U Attitude Determination and Control Subsystem (ADCS) are explo...
This paper presents a case study on the development of the Attitude Determination and Control System...
One of the challenges to date for operational spacecrafts is to satisfy high attitude pointing accur...
The design and test of a 6U CubeSat Attitude Determination and Control System (ADCS) are explored to...
The University of Illinois has developed the IlliniSat-2 CubeSat bus, a generic scalable and modular...
The University of Illinois has developed the IlliniSat-2 CubeSat bus, a generic scalable and modular...
The attitude determination and control system (ADCS) for a satellite is responsible for multiple key...
In this paper, the development of a performant and accurate Attitude Determination and Control Syste...
Since the beginning of space history new innovative ideas have been driving space scientists to deve...
Guidance, navigation, and control (GNC) systems are commonly found in vehicles, whether they be spac...
Spacecraft modularity is a powerful design methodology for shortening satellite development cycles a...
This thesis describes the development of the Attitude Determination and Control System (ADCS) for Cu...
In an attempt to reduce the cost of future satellites, new technologies are being pursued to develop...
The design and testing of AFIT\u27s 6U Attitude Determination and Control Subsystem (ADCS) are explo...
The design and testing of AFIT\u27s 6U Attitude Determination and Control Subsystem (ADCS) are explo...
The design and testing of AFIT\u27s 6U Attitude Determination and Control Subsystem (ADCS) are explo...
This paper presents a case study on the development of the Attitude Determination and Control System...
One of the challenges to date for operational spacecrafts is to satisfy high attitude pointing accur...
The design and test of a 6U CubeSat Attitude Determination and Control System (ADCS) are explored to...
The University of Illinois has developed the IlliniSat-2 CubeSat bus, a generic scalable and modular...
The University of Illinois has developed the IlliniSat-2 CubeSat bus, a generic scalable and modular...
The attitude determination and control system (ADCS) for a satellite is responsible for multiple key...
In this paper, the development of a performant and accurate Attitude Determination and Control Syste...
Since the beginning of space history new innovative ideas have been driving space scientists to deve...
Guidance, navigation, and control (GNC) systems are commonly found in vehicles, whether they be spac...
Spacecraft modularity is a powerful design methodology for shortening satellite development cycles a...