The design of a large angle three-axis attitude servomechanism for spacecraft
Design equations for large angle three-axis attitude servomechanism for controlling spacecraft
SPACECRAFT CONTROL↗
Engineering topics
Meyer, G.
Publications and source records attributed to Meyer, G..
On the use of Euler's theorem on rotations for the synthesis of attitude control systems
Euler theorem applied to rotations for synthesis of attitude control systems
ATTITUDE CONTROL↗
On the use of orthogonal transformation for the synthesis of attitude control systems.
Rigid body rotational attitude control in three dimensions with linear transformation as output variable, noting advantages, applications and results
LINEAR SYSTEM↗