The ability to stabilize a system and achieve performance objectives using
active feedback control is highly dependent on the location, quality, type,
and number of control actuators and sensors. One role of a control enginee
r is to interact with the system designer to locate, size, and determine th
e quality of actuators and sensors required for effective control. This pap
er addresses one of these issues: location of sensors based on closed-loop
objectives. A systematic approach, based on H-2 optimal control design tech
niques, is developed for sensor selection which achieves desired performanc
e objectives and includes system constraints. This approach is applied to t
he selection of sensors for active vibration attenuation on the NASA Langle
y Mini-Mast experimental structure.