op_point = operpoint('scdplane')
Operating Point for the Model scdplane.
(Time-Varying Components Evaluated at time t=0)
States:
(1.) scdplane/Actuator Model
x: 0
(2.) scdplane/Aircraft Dynamics Model/Transfer Fcn.1
x: 0
(3.) scdplane/Aircraft Dynamics Model/Transfer Fcn.2
x: 0
(4.) scdplane/Controller/Alpha-sensor Low-pass Filter
x: 0
(5.) scdplane/Controller/Pitch Rate Lead Filter
x: 0
(6.) scdplane/Controller/Proportional plus integral compensator
x: 0
(7.) scdplane/Controller/Stick Prefilter
x: 0
(8.) scdplane/Dryden Wind Gust Models/Q-gust model
x: 0
(9.) scdplane/Dryden Wind Gust Models/W-gust model
x: 0
x: 0
Inputs:
(1.) scdplane/u
u: 0
All states are initially set to 0.
Initialize the states in the operating point object to the values in xFinal. Set the input to
be 9.
newop = setxu(op_point,xFinal,9)
Operating Point for the Model scdplane.
(Time-Varying Components Evaluated at time t=0)
States:
(1.) scdplane/Actuator Model
setxu