1. 1Gyro, of the Aerospace, A. P., of the Institute of Electrical, E. S. S., and Engineers, E. “IEEE Standard Specification Format Guide and Test Procedure for Non-gyroscopic Inertial Angular Sensors Jerk, Acceleration, Velocity, and Displacement,” Ieee std 671-11985, 1985 (r2008), The Institute of Electrical and Electronics Engineers, Inc., New York, USA, 1985.
2. Improvements in flight table dynamic transparency for hardware-in-the-loop facilities
3. Robust Flight Control Using Incremental Nonlinear Dynamic Inversion and Angular Acceleration Prediction
4. Sensor-Based Backstepping