Asset Details
Do you wish to reserve the book?
Fast sliding mode control of aircraft ground lateral maneuver based on a double-integrator observer
Hey, we have placed the reservation for you!
By the way, why not check out events that you can attend while you pick your title.
Oops! Something went wrong.
Looks like we were not able to place the reservation. Kindly try again later.
Are you sure you want to remove the book from the shelf?
Fast sliding mode control of aircraft ground lateral maneuver based on a double-integrator observer
Do you wish to request the book?
Fast sliding mode control of aircraft ground lateral maneuver based on a double-integrator observer
Please be aware that the book you have requested cannot be checked out. If you would like to checkout this book, you can reserve another copy
We have requested the book for you!
Your request is successful and it will be processed during the Library working hours. Please check the status of your request in My Requests.
Oops! Something went wrong.
Looks like we were not able to place your request. Kindly try again later.
Journal Article
Fast sliding mode control of aircraft ground lateral maneuver based on a double-integrator observer
2026
Overview
Accurate yaw angle information is essential for reliable aircraft ground maneuver, but inertial measurements obtained during taxiing are often corrupted by high-frequency noise. To improve signal quality, a double-integrator observer is designed to reconstruct the yaw rate dynamics and attenuate measurement noise. Building on the refined state estimates, a fast sliding-mode controller is developed to achieve rapid and robust tracking of the reference yaw angle in the presence of model uncertainties. The proposed approach is validated through a six-degree-of-freedom aircraft simulation model.
Publisher
IOP Publishing
