Contributions to two nanosatellite missions are discussed. First, the design and development of a test system for an advanced nanosatellite power board is discussed. Details of software and hardware design process involved in the implementation of automated test procedures are presented. The system has been deployed for unit-level testing of power boards for several nanosatellite missions, significantly reducing testing cost and time. Next, a Mission Planning and Scheduling Software platform is proposed for Earth Observation missions. The motivation is described for the development of a stand-alone application enabling satellite operations teams to identify suitable observation scenario parameters. Attitude and orbital trajectory estimation...
Small satellites are growing in popularity because they offer an effective option that enables missi...
Recent science and technology advancements of micro and nanosatellites have opened possibilities for...
The development of a small spacecraft attitude determination and control subsystem is described. Th...
Contributions to two nanosatellite missions are discussed. First, the design and development of a te...
The analysis, verification and emulation of attitude control hardware for nanosatellite spacecraft i...
For spacecraft development, realizing strong supporting ground segment software is as important as d...
For spacecraft development, realizing strong supporting ground segment software is as important as d...
This thesis describes, in chronological order, the design and implementation of four separate ground...
This thesis describes, in chronological order, the design and implementation of four separate ground...
The adaptation of the University of Toronto Space Flight Laboratory Generic Nanosatellite Bus (GNB) ...
The Generic Nanosatellite Bus (GNB) is a spacecraft platform designed to accommodate the integration...
The adaptation of the University of Toronto Space Flight Laboratory Generic Nanosatellite Bus (GNB) ...
Nanosatellites represent an emerging opportunity to pursue a broad set of mission goals, including r...
ABSTRACT: This paper deals with the design and implementation of a fully capable ground station used...
Small satellites are growing in popularity because they offer an effective option that enables missi...
Small satellites are growing in popularity because they offer an effective option that enables missi...
Recent science and technology advancements of micro and nanosatellites have opened possibilities for...
The development of a small spacecraft attitude determination and control subsystem is described. Th...
Contributions to two nanosatellite missions are discussed. First, the design and development of a te...
The analysis, verification and emulation of attitude control hardware for nanosatellite spacecraft i...
For spacecraft development, realizing strong supporting ground segment software is as important as d...
For spacecraft development, realizing strong supporting ground segment software is as important as d...
This thesis describes, in chronological order, the design and implementation of four separate ground...
This thesis describes, in chronological order, the design and implementation of four separate ground...
The adaptation of the University of Toronto Space Flight Laboratory Generic Nanosatellite Bus (GNB) ...
The Generic Nanosatellite Bus (GNB) is a spacecraft platform designed to accommodate the integration...
The adaptation of the University of Toronto Space Flight Laboratory Generic Nanosatellite Bus (GNB) ...
Nanosatellites represent an emerging opportunity to pursue a broad set of mission goals, including r...
ABSTRACT: This paper deals with the design and implementation of a fully capable ground station used...
Small satellites are growing in popularity because they offer an effective option that enables missi...
Small satellites are growing in popularity because they offer an effective option that enables missi...
Recent science and technology advancements of micro and nanosatellites have opened possibilities for...
The development of a small spacecraft attitude determination and control subsystem is described. Th...