Adaptive Compensation of Aerodynamic Effects during Takeoff and Landing Manoeuvres for a Scale Model Autonomous Helicopter
References (32)
- et al.
Nonlinear control design for slightly non-minimum phase systems: Applications to v/stol aircraft
Automatica
(1992) - et al.
A different look at output tracking: control of a VTOL aircraft
Auto matica
(1996) - Amida O. An autonomous vision-guided helicopter. PhD thesis, Electrical and Computer Engineering Department, Carnegie...
- Bradley R. The flying brick exposed: nonlinear control of a basic helicopter model. Technical Report TR/MATI RB/6,...
- et al.
Trajectory tracking control design for autonomous helicopters using a backstepping algorithm
- et al.
Sensitivity of helicopter aeromechanical stability to dynamic inflow
Vertica
(1982) Nonlinear control system design via dynamic order reduction
- et al.
Adaptive systems with reduced models
(1983) - et al.
Systematic design of adaptive controllers for feedback linearizable systems
IEEE Trans Autom Control
(1991) - et al.
Trajectory initialisation in adaptive nonlinear control
Output tracking control design of a helicopter model based on approximate lineariza tion
Non linear and adaptive control design
(1995)
Helicopter control design using feedback linearization techniques
Proceedings of the 28th conference on decision and control, CDC’89
p
(1989)
A new notion of persitency-of-excitation for UGAS of NLTV systems: applicaton to stabilisation of nonholonomic systems
Hover control via approximate lyapunov control for a model helicopter
(Almost) exact path tracking control for an autonomous helicopter in hover manoeuvres
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2024, European Journal of ControlPosition tracking control of a helicopter in ground effect using nonlinear disturbance observer-based incremental backstepping approach
2018, Aerospace Science and TechnologyCitation Excerpt :As demonstrated in [11,12], the aerodynamic nature of ground effect is unsteady and highly nonlinear, which makes the design of a helicopter FCS challenging. At present, there have been limited analysis dedicated to controller designs of a helicopter operating in ground effect, and the relevant control approaches include adaptive backstepping [13,14], sliding mode control [15], LQR [16,17], H2 state feedback control [18] and H∞ state feedback control [19]. Although simulation experiments verified the effectiveness of the proposed control approaches, several problems with these studies are summarized as follows:
Performing and extending aggressive maneuvers using iterative learning control
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2011, International Journal of Micro Air VehiclesRos-Gazebo Based Virtual PVTOL Experimental Platform to Validate Control Algorithms
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2021, 2021 International Conference on Unmanned Aircraft Systems, ICUAS 2021
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