Add to ORKGHigh-accuracy pointing capabilities are desired for many three-axis stabilized small satellites. Momentum-based attitude control system actuators, initially developed for larger satellites, are being utilized by small satellites to meet these pointing requirements. This paper provides an overview of momentum devices available for small satellite applications and three-axis attitude control system (ACS) configurations using these devices. Factors affecting the selection and sizing of ACS components are also addressed. Included are suggestions for potential ACS improvements and cost-saving measures that will make momentum devices more accessible to the small satellite community
Advancing technology has allowed for the development of low cost attitude control hardware for micro...
As technology improves, increasingly higher resolution payload can be achieved using Cubesats for Ea...
Nowadays, most of the designed satellites are dedicated for high performance missions, which require...
A design study of the attitude control system for the High Energy Transient Experiment (RETE) small ...
This paper addresses the problem of the momentum dumping for the pitch momentum wheel onboard ALMASa...
This paper addresses the problem of the momentum dumping for the pitch momentum wheel onboard ALMASa...
This paper addresses the problem of the momentum dumping for the pitch momentum wheel onboard ALMASa...
In order to meet the cost goals of small satellites, attitude determination and control problems mus...
In order to meet the cost goals of small satellites, attitude determination and control problems mus...
The move towards miniaturizing satellites will not be based solely on scaling down with a commensura...
This paper provides an overview of the on-orbit operation of the Attitude Control Subsystem (ACS) fo...
Abstract. The move towards miniaturizing satellites will not be based solely on scaling down with a ...
In an attempt to reduce the cost of future satellites, new technologies are being pursued to develop...
Abstract: In this paper a new practical Attitude Control System is proposed, based on Control Momen...
textA flexible, robust attitude determination and control (ADC) system is presented for small satell...
Advancing technology has allowed for the development of low cost attitude control hardware for micro...
As technology improves, increasingly higher resolution payload can be achieved using Cubesats for Ea...
Nowadays, most of the designed satellites are dedicated for high performance missions, which require...
A design study of the attitude control system for the High Energy Transient Experiment (RETE) small ...
This paper addresses the problem of the momentum dumping for the pitch momentum wheel onboard ALMASa...
This paper addresses the problem of the momentum dumping for the pitch momentum wheel onboard ALMASa...
This paper addresses the problem of the momentum dumping for the pitch momentum wheel onboard ALMASa...
In order to meet the cost goals of small satellites, attitude determination and control problems mus...
In order to meet the cost goals of small satellites, attitude determination and control problems mus...
The move towards miniaturizing satellites will not be based solely on scaling down with a commensura...
This paper provides an overview of the on-orbit operation of the Attitude Control Subsystem (ACS) fo...
Abstract. The move towards miniaturizing satellites will not be based solely on scaling down with a ...
In an attempt to reduce the cost of future satellites, new technologies are being pursued to develop...
Abstract: In this paper a new practical Attitude Control System is proposed, based on Control Momen...
textA flexible, robust attitude determination and control (ADC) system is presented for small satell...
Advancing technology has allowed for the development of low cost attitude control hardware for micro...
As technology improves, increasingly higher resolution payload can be achieved using Cubesats for Ea...
Nowadays, most of the designed satellites are dedicated for high performance missions, which require...