It is important to establish system dynamic model for many fields
especially in the fields of adaptive control and failure monitor of advanced aero engine.Many identification methods were used for this problem
including AR
OE
and so on.Numerical algorithm for subspace state space system identification (N4SID) is proposed in recent years and applied to communications.It is based on state space model.N4SID is described in this paper.Though areo engine is a complex non linear system
at "little bias" state
the model is linear time invariable system.In this paper
N4SID is applied to identifying aero thermal model of a certain double spool turbojet aero engine at "little bias" state.Moreover
the result shows us that this algorithm is feasible.