Designing Stipulated Gains of Aircraft Stability and Control Augmentation Systems for Semiglobal Trajectories Tracking

Table 3

Magnitude of sensor noise standard deviations.

Parameter	Standard deviation
Airspeed indicator	11 ft/sec
Roll rate gyro	0.14 deg/sec
Pitch rate gyro	0.14 deg/sec
Yaw rate gyro	0.14 deg/sec
Longitudinal accelerometer	0.98 ft/sec^2
Lateral accelerometer	0.98 ft/sec^2
Directional accelerometer	0.98 ft/sec^2
Attitude pitch gyro	0.573 deg
Attitude roll gyro	0.573 deg
Attitude yaw gyro	0.573 deg
Altitude rate indicator	0.25 ft/sec
Altitude indicator	10 ft
Angle of attack	0.1 deg
Sideslip angle	0.1 deg