Finite-time path following control for a stratospheric airship with input saturation and error constraint
Author:
Affiliation:
1. The Seventh Research Division, School of Automation Science and Electrical Engineering, Beihang University , Beijing, P.R. China
2. School of Electrical and Electronic Engineering, Nanyang Technological University , Singapore
Funder
National Natural Science Foundation of China
Aeronautical Science Foundation of China
National Key R&D Program of China
Fundamental Research Funds for the Central Universities
China Scholarship Council
Publisher
Informa UK Limited
Subject
Computer Science Applications,Control and Systems Engineering
Link
https://www.tandfonline.com/doi/pdf/10.1080/00207179.2017.1357839
Reference67 articles.
1. Dynamic modeling of the airship with Matlab using geometrical aerodynamic parameters
2. Airship Hover Stabilization Using a Backstepping Control Approach
3. A backstepping controller for path-tracking of an underactuated autonomous airship
4. Tracking control of trim trajectories of a blimp for ascent and descent flight manoeuvres
5. Integral Line-of-Sight Guidance and Control of Underactuated Marine Vehicles: Theory, Simulations, and Experiments
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