spec: dx = 0, initial guess: 0
spec: dx = 0, initial guess: -3.05e+03
(2.) scdairframe/EOM/ Equations of Motion (Body Axes)/Theta
spec: dx = 0, initial guess: 0
(3.) scdairframe/EOM/ Equations of Motion (Body Axes)/U,w
spec: dx = 0, initial guess: 984
spec: dx = 0, initial guess: 0
(4.) scdairframe/EOM/ Equations of Motion (Body Axes)/q
spec: dx = 0, initial guess: 0
Inputs:
(1.) scdairframe/Fin Deflection
initial guess: 0
Outputs:
(1.) scdairframe/q
spec: none
(2.) scdairframe/az
spec: none
First, we set the Position state specifications, which are known but not at steady state:
opspec.States(1).Known = [1;1];
opspec.States(1).SteadyState = [0;0];
The second state specification is Theta which is known but not at steady state:
opspec.States(2).Known = 1;
opspec.States(2).SteadyState = 0;
The third state specification includes the body axis angular rates where the variable w is
at steady state:
opspec.States(3).Known = [1 1];
opspec.States(3).SteadyState = [0 1];
Next, we search for the operating point that meets this specification.
op = findop('scdairframe',opspec);
Operating point search report:
Trimming and Linearizing an Airframe