A laboratory facility for the study of control laws for large flexible spacecraft is described. The facility fulfills the requirements of the Spacecraft Control Laboratory Experiment (SCOLE) design challenge for a laboratory experiment, which will allow slew maneuvers and pointing operations. The structural apparatus is described in detail sufficient for modelling purposes. The sensor and actuator types and characteristics are described so that identification and control algorithms may be designed. The control implementation computer and real-time subroutines are also described
This is the first of two reports on the dynamics and control of slewing maneuvers of the NASA Spacec...
NASA Marshall Space Flight Center has developed a facility in which closed loop control of Large Spa...
An overview of space oriented control technology programs which are applicable to flexible large spa...
The Spacecraft Control Laboratory Experiment (SCOLE) was conceived to provide a physical test bed fo...
The problen of controlling large, flexible space systems has been evaluated using computer simulatio...
An NASA program is discussed which was initiated to make direct comparisons of control laws for, fir...
A stereo camera tracking system was developed to provide a near real-time measure of the position an...
Work during the period January 1 to June 30, 1985 has concentrated on the completion of the derivati...
This is the final report on the dynamics and control of slew maneuvers of the Spacecraft Control Lab...
A mathematical model is developed to predict the dynamics of the proposed orbiting Spacecraft Contro...
This is the second report of a set of two reports on the dynamics and control of slewing maneuvers o...
The dynamics and control of slewing maneuvers of NASA Spacecraft COntrol Laboratory Experiment (SCOL...
A brief survey of large space structure control related experiments and facilities was presented. Th...
An experimental structure is described which was constructed to demonstrate and validate recent emer...
The dynamics and control of slewing maneuvers of a large flexible spacecraft, namely, NASA Spacecraf...
This is the first of two reports on the dynamics and control of slewing maneuvers of the NASA Spacec...
NASA Marshall Space Flight Center has developed a facility in which closed loop control of Large Spa...
An overview of space oriented control technology programs which are applicable to flexible large spa...
The Spacecraft Control Laboratory Experiment (SCOLE) was conceived to provide a physical test bed fo...
The problen of controlling large, flexible space systems has been evaluated using computer simulatio...
An NASA program is discussed which was initiated to make direct comparisons of control laws for, fir...
A stereo camera tracking system was developed to provide a near real-time measure of the position an...
Work during the period January 1 to June 30, 1985 has concentrated on the completion of the derivati...
This is the final report on the dynamics and control of slew maneuvers of the Spacecraft Control Lab...
A mathematical model is developed to predict the dynamics of the proposed orbiting Spacecraft Contro...
This is the second report of a set of two reports on the dynamics and control of slewing maneuvers o...
The dynamics and control of slewing maneuvers of NASA Spacecraft COntrol Laboratory Experiment (SCOL...
A brief survey of large space structure control related experiments and facilities was presented. Th...
An experimental structure is described which was constructed to demonstrate and validate recent emer...
The dynamics and control of slewing maneuvers of a large flexible spacecraft, namely, NASA Spacecraf...
This is the first of two reports on the dynamics and control of slewing maneuvers of the NASA Spacec...
NASA Marshall Space Flight Center has developed a facility in which closed loop control of Large Spa...
An overview of space oriented control technology programs which are applicable to flexible large spa...