Operating point specification for the Model csthl20_trim.
(Time-Varying Components Evaluated at time t=0)
States:
(1.) csthl20_trim/HL20 Airframe/6DOF (Euler Angles)/Calculate DCM & Euler Angles/phi theta psi
spec: dx = 0, initial guess: 0
spec: dx = 0, initial guess: -0.199
spec: dx = 0, initial guess: 0
(2.) csthl20_trim/HL20 Airframe/6DOF (Euler Angles)/p,q,r
spec: dx = 0, initial guess: 0
spec: dx = 0, initial guess: 0
spec: dx = 0, initial guess: 0
(3.) csthl20_trim/HL20 Airframe/6DOF (Euler Angles)/ub,vb,wb
spec: dx = 0, initial guess: 203
spec: dx = 0, initial guess: 0
spec: dx = 0, initial guess: 23.3
(4.) csthl20_trim/HL20 Airframe/6DOF (Euler Angles)/xe,ye,ze
spec: dx = 0, initial guess: -1.21e+04
spec: dx = 0, initial guess: 0
spec: dx = 0, initial guess: -3.05e+03
Inputs:
(1.) csthl20_trim/da
initial guess: 0
(2.) csthl20_trim/de
initial guess: 0
(3.) csthl20_trim/dr
initial guess: 0
Outputs:
(1.) csthl20_trim/p;q;r (1-3)
spec: none
spec: none
spec: none
(2.) csthl20_trim/phi;theta;psi (4-6)
spec: none
spec: none
spec: none
(3.) csthl20_trim/alpha (7)
spec: none
Trimming and Linearization of the HL-20 Airframe