Add to ORKGVarious three axis bang-bang control laws were implemented on the Small Satellite Attitude Control Simulator (SSACS) table. The optimal time control law\u27s experimental results demonstrated excellent correlation with the desired switching curve. Approximately 55.6% less fuel will be used for a given maneuver if the optimal time control law is modified to shut the thrusters off when the magnitude of the angular velocity reaches 1 deg/sec in the appropriate region; however, the time required to perform the maneuver increases. These results demonstrate the SSACS table\u27s capability to simulate the attitude dynamics of small satellites
This work presents the first known energy storage and attitude control subsystem (ESACS) for small s...
In this work, we design, build, and test two 1.25U CubeSats. These small satellites were deployed on...
AFIT/GA/ENY/09-M06 Optimization of spacecraft attitude maneuvers can significantly reduce attitude c...
Utah State University has developed an air bearing table to simulate the attitude dynamics of a smal...
Utah State University has developed an air bearing table to simulate the attitude dynamics of a smal...
The physical environment of a space vehicle shows that bang-bang method for attitude control system ...
The design of most hardware-based spacecraft attitude simulators restricts motion in one or more axe...
In this research, the attitude determination and control system (ADCS) of a small satellite is exami...
Abstract: In this paper a new practical Attitude Control System is proposed, based on Control Momen...
AbstractAgile satellites are of importance in modern aerospace applications, but high mobility of th...
Nowadays, most of the designed satellites are dedicated for high performance missions, which require...
Abstract. Within the motto smaller, cheaper and better, several nations can have now easy access to ...
Agile satellites are of importance in modern aerospace applications, but high mobility of the satell...
Different attitude control strategies of a small satellite are presented in this paper as well as th...
Attitude control of a satellite is required for the pointing of communications antennas and other in...
This work presents the first known energy storage and attitude control subsystem (ESACS) for small s...
In this work, we design, build, and test two 1.25U CubeSats. These small satellites were deployed on...
AFIT/GA/ENY/09-M06 Optimization of spacecraft attitude maneuvers can significantly reduce attitude c...
Utah State University has developed an air bearing table to simulate the attitude dynamics of a smal...
Utah State University has developed an air bearing table to simulate the attitude dynamics of a smal...
The physical environment of a space vehicle shows that bang-bang method for attitude control system ...
The design of most hardware-based spacecraft attitude simulators restricts motion in one or more axe...
In this research, the attitude determination and control system (ADCS) of a small satellite is exami...
Abstract: In this paper a new practical Attitude Control System is proposed, based on Control Momen...
AbstractAgile satellites are of importance in modern aerospace applications, but high mobility of th...
Nowadays, most of the designed satellites are dedicated for high performance missions, which require...
Abstract. Within the motto smaller, cheaper and better, several nations can have now easy access to ...
Agile satellites are of importance in modern aerospace applications, but high mobility of the satell...
Different attitude control strategies of a small satellite are presented in this paper as well as th...
Attitude control of a satellite is required for the pointing of communications antennas and other in...
This work presents the first known energy storage and attitude control subsystem (ESACS) for small s...
In this work, we design, build, and test two 1.25U CubeSats. These small satellites were deployed on...
AFIT/GA/ENY/09-M06 Optimization of spacecraft attitude maneuvers can significantly reduce attitude c...