System identification is often a precursor to model-based control system de
signs that assume the plant dynamics to be controlled are known. Many syste
m identification algorithms, such as Observer Kalman Filter Identification
(OKID), do not guarantee that the identified model will be stable and when
applied to flexible structures that exhibit rigid modes, the identified mod
els are often unstable. These unstable models can create problems for model
validation and subsequent model order reduction for control design. By exp
onentially curve fitting the unstable Markov parameters generated by OKID,
this instability can be effectively identified and removed allowing stable
models to be identified. This system identification technique is validated
by computer simulation as well as experimentally using the Dynamics Identif
ication and Control Experiment (DICE), a flexible spacecraft emulator desig
ned to fly on the NASA space shuttle.