Simulink Control Design™ - MathWorks

(4.) scdairframeTRIM/Airframe Model/EOM/ Equations of Motion (Body Axes)/q

x: 0 dx: 31.2 (0)

Inputs:

----------

(1.) scdairframeTRIM/delta

u: 0 [-Inf Inf]

Outputs:

----------

(1.) scdairframeTRIM/alpha

y: -0.21 [-Inf Inf]

(2.) scdairframeTRIM/V

y: 933 [-Inf Inf]

(3.) scdairframeTRIM/q

y: 0 [-Inf Inf]

(4.) scdairframeTRIM/az

y: 263 [-Inf Inf]

(5.) scdairframeTRIM/gamma

y: 0.21 [-Inf Inf]

In the operating point search report, the dx values for the specified steady states have

zero constraints, as indicated by the 0 value in parentheses. The optimization search did

not find a steady-state operating point, since all three of these states violate the

constraints.

See Also

Functions

findop | findopOptions

Apps

Linear Analysis Tool | Steady State Manager

More About

• “Compute Operating Points from Specifications at the Command Line” on page 1-17


• “Compute Operating Points from Specifications Using Steady State Manager” on
  page 1-23

1 Steady-State Operating Points