Таблица начальных условий
Angle of attack | 2,19 |
Pressure altitude | 15899,67 |
Indicated airspeed | 288,02 |
Roll Euler angle | -0,14 |
Pitch Euler angle | 6,18 |
Vertical speed indication | 2547,67 |
Left-right stab trim indicator | -2,78 |
Engine N1 | 98,49 |
Elevator deflection | 0,75 |
Aileron deflection | -0,19 |
Rudder deflection | 0,00 |
Absolute value of sideslip angle | 0,00 |
Speed Brake Position - Variable | 0,00 |
Windshear active flag | 0,00 |
Aircraft upset active | 0,00 |
Roll Rate | 0,05 |
Pitch Rate | 0,00 |
Yaw Rate | -0,01 |
N2RPM Engine N2 | 98,49 |
N1RPM Engine N1 | 98,49 |
Vertical deviation from glidepath | 0,00 |
Horizontal deviation | 0,00 |
Roll acceleration - Body axis | 0,00 |
Pitch acceleration - Body axis | 0,00 |
Yaw acceleration - Body axis | 0,00 |
Roll Acceleration | 0,00 |
Pitch Acceleration | 0,00 |
Yaw Acceleration | 0,00 |