GSP internally represents a gas turbine engine system model as a 'virtual' set of non-linear differential equations. GSP's generic solver solves these equations in order to find a valid steady state or transient operating point (for more information see the Technical Manual and Reference [4].
The number of states and/or errors is affected by the Component model options for the following components:
•Fan
•Compressor
•Turbine
•Manual fuel control
•Gas generator fuel control,
•Turboshaft fuel control
Failure of correct setting of the Component model options affecting the states and error configuration of the model will be reported as either an error due to the number of model states and (equation) errors not being equal or an error detecting more than one component trying to (user) specify the same shaft.
Component states and errors
