Add to ORKGBaseline system definition of attitude control for small satellites and related subsystem
A small angle stability analysis is presented for one particular configuration of a high power commu...
textA flexible, robust attitude determination and control (ADC) system is presented for small satell...
Utah State University has developed an air bearing table to simulate the attitude dynamics of a smal...
Engineering studies of attitude control of small satellites and related subsystem
System concepts were characterized in order to define cost versus benefits for autonomous functional...
Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2011.Ca...
Mathematical analyses of suboptimal attitude maneuvering control for synchronous earth pointing sate...
This paper provides an overview of the on-orbit operation of the Attitude Control Subsystem (ACS) fo...
In an attempt to reduce the cost of future satellites, new technologies are being pursued to develop...
The world of satellites is evolving very rapidly on the past few years, with satellites going from h...
Progress reports on guidance and attitude control mechanisms of different flight vehicles are presen...
Msti2 is a small, 164 kg (362 lb), 3-axis stabilized, low-Earth-orbiting satellite whose mission is ...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1991.In...
The development of a small spacecraft attitude determination and control subsystem is described. Th...
High-accuracy pointing capabilities are desired for many three-axis stabilized small satellites. Mom...
A small angle stability analysis is presented for one particular configuration of a high power commu...
textA flexible, robust attitude determination and control (ADC) system is presented for small satell...
Utah State University has developed an air bearing table to simulate the attitude dynamics of a smal...
Engineering studies of attitude control of small satellites and related subsystem
System concepts were characterized in order to define cost versus benefits for autonomous functional...
Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2011.Ca...
Mathematical analyses of suboptimal attitude maneuvering control for synchronous earth pointing sate...
This paper provides an overview of the on-orbit operation of the Attitude Control Subsystem (ACS) fo...
In an attempt to reduce the cost of future satellites, new technologies are being pursued to develop...
The world of satellites is evolving very rapidly on the past few years, with satellites going from h...
Progress reports on guidance and attitude control mechanisms of different flight vehicles are presen...
Msti2 is a small, 164 kg (362 lb), 3-axis stabilized, low-Earth-orbiting satellite whose mission is ...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1991.In...
The development of a small spacecraft attitude determination and control subsystem is described. Th...
High-accuracy pointing capabilities are desired for many three-axis stabilized small satellites. Mom...
A small angle stability analysis is presented for one particular configuration of a high power commu...
textA flexible, robust attitude determination and control (ADC) system is presented for small satell...
Utah State University has developed an air bearing table to simulate the attitude dynamics of a smal...