Not to be confused with Sideslip angle.
Not to be confused with Yaw rate.
The yaw angle is the angle between a vehicle's heading and a reference heading (normally true or magnetic North). One of the Tait-Bryan angles. In aeronautics, robotics and marine control, it is typically assigned the shorthand notation ψ.[1]
- Further information: Flight dynamics
And for Automotive vehicle control
- Further information: Electronic stability control
[edit] References
- ^ Hurt, H. H., Jr. (January 1965) [1960]. Aerodynamics for Naval Aviators. U.S. Government Printing Office, Washington D.C.: U.S. Navy, Aviation Training Division. p. 284. NAVWEPS 00-80T-80.
All text is available under the terms of the GNU Free Documentation License. (See Copyrights for details.)
Wikipedia® is a registered trademark of the Wikimedia Foundation, Inc.
Privacy policy - About Wikipedia - Disclaimers - Fundraising

