23,99 €
inkl. MwSt.
Versandfertig in 6-10 Tagen
12 °P sammeln
Andere Kunden interessierten sich auch für
![An innovative control of ship list/roll by active U-tank]( "An innovative control of ship list/roll by active U-tank")
An innovative control of ship list/roll by active U-tank23,99 €![Direct Torque Control of IPMSMs by Nonlinear Optimal Control Technique]( "Direct Torque Control of IPMSMs by Nonlinear Optimal Control Technique")
Direct Torque Control of IPMSMs by Nonlinear Optimal Control Technique32,99 €![Nonlinear Optimal Model Following Control of Flexible Aircraft]( "Nonlinear Optimal Model Following Control of Flexible Aircraft")
Nonlinear Optimal Model Following Control of Flexible Aircraft51,99 €![Nonlinear Adaptive Flight Control System for Unmanned Aerial Vehicle]( "Nonlinear Adaptive Flight Control System for Unmanned Aerial Vehicle")
Nonlinear Adaptive Flight Control System for Unmanned Aerial Vehicle32,99 €![New Approach and Results on the Stability and Control of Airship]( "New Approach and Results on the Stability and Control of Airship")
New Approach and Results on the Stability and Control of Airship44,99 €![Incorporating Input Saturation For Underactuated Surface Vessel Trajec]( "Incorporating Input Saturation For Underactuated Surface Vessel Trajec")
Incorporating Input Saturation For Underactuated Surface Vessel Trajec36,99 €![Nonlinear H¿ Guidance Design for Missile via Galerkin Approximation]( "Nonlinear H¿ Guidance Design for Missile via Galerkin Approximation")
Nonlinear H¿ Guidance Design for Missile via Galerkin Approximation36,99 €
This book proposes a new trajectory tracking control approach for an underactuated stratospheric airship. There is a two-level structure of the proposed controller. A low-level controller based on nonlinear backstepping method, with the rigid body dynamics expressed on vector form, stabilizes the attitude and velocity of the airship, while a high-level controller performs guidance and trajectory tracking task in the three dimensional (3-D) space. Furthermore, a control allocation module based on active set algorithm is incorporated into the low-level controller to optimize the practical control inputs under constraints of actuator saturation. The closed-loop trajectory tracking control plant is proved to be globally exponentially stable through Lyapunov theory. Finally, simulations show that nonlinear backstepping trajectory tracking controller can achieve desired tracking performances even if the airship is affected by time delay inputs and exogenous disturbances.