This paper proposes an adaptive backstepping sliding mode flight control method that is compatible with heavyweight cargo airdrop. The goal is to maintain the plane states during cargo extraction process, in the presence of uncertainties of both constant and time-varying types, as well as matched and unmatched types. A backstepping sliding mode flight control law with parameter adaptation is presented based on the plane-cargo dynamics in strict-feedback form. The control approach consists in having an adaptation law that approximates the disturbance and uncertain aerodynamic function, which is separated from the complex nonlinearities. Also, the adaptation algorithm with projection can bound the estimated function. This ensures the robustne...
This paper presents an incremental backstepping sliding-mode (IBS) controller for trajectory control...
Fault-tolerant flight control has the potential of improving the aircraft survivability in real life...
A nonlinear constrained controller is designed for a reusable launch vehicle during re-entry phase i...
This paper proposes an adaptive backstepping sliding mode flight control method that is compatible w...
An autopilot inner loop that combines backstepping control with adaptive function approximation is d...
AbstractDuring airdrop of heavy load, the flight parameters vary continuously as the load moves in t...
AbstractThe nonlinear aircraft model with heavy cargo moving inside is derived by using the separati...
AbstractThe nonlinear aircraft model with heavy cargo moving inside is derived by using the separati...
The nonlinear aircraft model with heavy cargo moving inside is derived by using the separation body ...
The longitudinal nonlinear aircraft model with cargo extraction is derived using theoretical mechani...
In view of the strong nonlinear and coupling characteristics of the airdrop operations, a novel cont...
In view of the strong nonlinear and coupling characteristics of the airdrop operations, a novel cont...
AbstractThe mathematical model of a transport aircraft would be subjected to a sudden change when he...
AbstractCargo airdrop has long been one of the most important measures to deal with urgent immediate...
The main goal of this thesis is to investigate the potential of the nonlinear adaptive backstepping ...
This paper presents an incremental backstepping sliding-mode (IBS) controller for trajectory control...
Fault-tolerant flight control has the potential of improving the aircraft survivability in real life...
A nonlinear constrained controller is designed for a reusable launch vehicle during re-entry phase i...
This paper proposes an adaptive backstepping sliding mode flight control method that is compatible w...
An autopilot inner loop that combines backstepping control with adaptive function approximation is d...
AbstractDuring airdrop of heavy load, the flight parameters vary continuously as the load moves in t...
AbstractThe nonlinear aircraft model with heavy cargo moving inside is derived by using the separati...
AbstractThe nonlinear aircraft model with heavy cargo moving inside is derived by using the separati...
The nonlinear aircraft model with heavy cargo moving inside is derived by using the separation body ...
The longitudinal nonlinear aircraft model with cargo extraction is derived using theoretical mechani...
In view of the strong nonlinear and coupling characteristics of the airdrop operations, a novel cont...
In view of the strong nonlinear and coupling characteristics of the airdrop operations, a novel cont...
AbstractThe mathematical model of a transport aircraft would be subjected to a sudden change when he...
AbstractCargo airdrop has long been one of the most important measures to deal with urgent immediate...
The main goal of this thesis is to investigate the potential of the nonlinear adaptive backstepping ...
This paper presents an incremental backstepping sliding-mode (IBS) controller for trajectory control...
Fault-tolerant flight control has the potential of improving the aircraft survivability in real life...
A nonlinear constrained controller is designed for a reusable launch vehicle during re-entry phase i...