Velocity-Aided Attitude Estimation for Helicopter Aircraft Using Microelectromechanical System Inertial-Measurement Units.

Velocity-Aided Attitude Estimation for Helicopter Aircraft Using Microelectromechanical System Inertial-Measurement Units. — المؤلف: Lee, Sang Cheol — Sensors (Basel, Switzerland) 20180124

المؤلف
Lee, Sang Cheol
النشر
Sensors (Basel, Switzerland) 20180124