A simple nonlinear stabilization control of planar vertical take-off and landing aircraft based on finite-time control and controlled Lagrangians
From MaRDI portal
Publication:6578870
DOI10.1002/ASJC.2584MaRDI QIDQ6578870
Publication date: 25 July 2024
Published in: Asian Journal of Control (Search for Journal in Brave)
Cites Work
- A backstepping-based procedure with saturation functions to control the PVTOL system
- Nonlinear control design for slightly non-minimum phase systems: Application to V/STOL aircraft
- Geometric homogeneity with applications to finite-time stability
- Finite-time observer-based output-feedback control for the global stabilisation of the PVTOL aircraft with bounded inputs
- Global stabilisation of the PVTOL aircraft with lateral force coupling and bounded inputs
- Minimum energy oriented global stabilizing control of the PVTOL aircraft
- Global stabilization of a PVTOL aircraft model with bounded inputs
- Finite-Time Stability of Continuous Autonomous Systems
- Robust Trajectory‐Tracking Control of a PVTOL under Crosswind
- Global configuration stabilization for the VTOL aircraft with strong input coupling
- Interconnection and damping assignment passivity-based control of mechanical systems with underactuation degree one
- Robust Stabilization of Nonlinear PVTOL Aircraft with Parameter Uncertainties
- An Alternative Nonlinear Control Law for the Global Stabilization of the PVTOL Vehicle
- A prediction‐based nonlinear controller for stabilization of a non‐minimum phase PVTOL aircraft
- Autonomous vertical landing on an oscillating platform: An internal-model based approach
- Control of VTOL aircraft with position state constraints using the barrier Lyapunov function
Related Items (1)
This page was built for publication: A simple nonlinear stabilization control of planar vertical take-off and landing aircraft based on finite-time control and controlled Lagrangians
Report a bug (only for logged in users!)Click here to report a bug for this page (MaRDI item Q6578870)
