Identification of a MIMO state space model of an F/A-18 aircraft using a subspace method
نویسندگان
چکیده
H altitude or impulse response matrix I identity matrix j dummy index M Mach number R correlation coefficient S matrix of singular values STBL left stabiliser position STBR right stabiliser position t, Δt time, time step T projected state matrix multiplied by the instrument TEFL left trailing-edge flap deflection TEFR right trailing-edge flap deflection u system input vector U matrix of past or future inputs or matrix of singular vector v perturbation vector on the system outputs V future noise effect matrix or matrix of singular vector Var variance Vec operation which organises the parameters of a matrix into a column vector VERTL left rudder position VERTR right rudder position w perturbation vector on the system states W weight matrix WINGL left wing deflection WINGR right wing deflection x system state vector ABSTRACT
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