Analysis of a wheel-damped reaction boom control system
Hybrid satellite attitude control system deformation model, utilizing pivoted flexible boom with tip mass as actuator and inertia wheels to dampen gravity induced librations
Buckingham, A. G.↗
Engineering topics
Publications and source records attributed to Buckingham, A. G..
Hybrid satellite attitude control system deformation model, utilizing pivoted flexible boom with tip mass as actuator and inertia wheels to dampen gravity induced librations
Torqued two axis gimbaled boom actuator satellite attitude control
Torqued two axis gimbaled boom actuator satellite attitude control