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Journal Articles
Accepted Manuscript
Article Type: Research-Article
J. Dyn. Sys., Meas., Control.
Paper No: DS-22-1029
Published Online: January 28, 2023
Journal Articles
Accepted Manuscript
Article Type: Research-Article
J. Dyn. Sys., Meas., Control.
Paper No: DS-22-1137
Published Online: January 28, 2023
Journal Articles
Accepted Manuscript
Article Type: Research-Article
J. Dyn. Sys., Meas., Control.
Paper No: DS-22-1194
Published Online: January 20, 2023
Journal Articles
Accepted Manuscript
Article Type: Technical Briefs
J. Dyn. Sys., Meas., Control.
Paper No: DS-22-1168
Published Online: January 20, 2023
Journal Articles
Article Type: Research-Article
J. Dyn. Sys., Meas., Control. April 2023, 145(4): 041002.
Paper No: DS-22-1142
Published Online: January 13, 2023
Image
in Energy-Optimal Unmanned Aerial Vehicles Motion Planning and Control Based on Integrated System Physical Dynamics
> Journal of Dynamic Systems, Measurement, and Control
Published Online: January 13, 2023
Fig. 1 Rotor subsystem schematics: ( a ) geometries of a blade cross section and ( b ) propeller flow stream More
Image
in Energy-Optimal Unmanned Aerial Vehicles Motion Planning and Control Based on Integrated System Physical Dynamics
> Journal of Dynamic Systems, Measurement, and Control
Published Online: January 13, 2023
Fig. 2 Equivalent circuit diagrams of ( a ) motor-ESC model and ( b ) battery model More
Image
in Energy-Optimal Unmanned Aerial Vehicles Motion Planning and Control Based on Integrated System Physical Dynamics
> Journal of Dynamic Systems, Measurement, and Control
Published Online: January 13, 2023
Fig. 3 Layout of rotors, axes, and torques (inset: axis orientations) More
Image
in Energy-Optimal Unmanned Aerial Vehicles Motion Planning and Control Based on Integrated System Physical Dynamics
> Journal of Dynamic Systems, Measurement, and Control
Published Online: January 13, 2023
Fig. 4 Block diagram of integrated system model More
Image
in Energy-Optimal Unmanned Aerial Vehicles Motion Planning and Control Based on Integrated System Physical Dynamics
> Journal of Dynamic Systems, Measurement, and Control
Published Online: January 13, 2023
Fig. 5 Rotor efficiency (output thrust per unit input power from motor) versus rotor angular velocity at V b = 25 V More
Image
in Energy-Optimal Unmanned Aerial Vehicles Motion Planning and Control Based on Integrated System Physical Dynamics
> Journal of Dynamic Systems, Measurement, and Control
Published Online: January 13, 2023
Fig. 6 Energy used per meter over a range of cruise velocities with and without wind at V b = 23 V More
Image
in Energy-Optimal Unmanned Aerial Vehicles Motion Planning and Control Based on Integrated System Physical Dynamics
> Journal of Dynamic Systems, Measurement, and Control
Published Online: January 13, 2023
Fig. 7 Two-level feedback control architecture, including high-level PID control to generate intermediate commands and low-level PID control to generate throttle and angular acceleration commands More
Image
in Energy-Optimal Unmanned Aerial Vehicles Motion Planning and Control Based on Integrated System Physical Dynamics
> Journal of Dynamic Systems, Measurement, and Control
Published Online: January 13, 2023
Fig. 8 Trajectories of key UAV states under each controller in simulation for forward ( X f =100 m, Z f = 0m) and diagonal ( X f = 50m, Z f = 20m) flights: ( a ) X position of forward flight, ( b ) X velocity of forward flight, ( c ) pitch angle of forward flight, ( d ) Z position ... More
Image
in Energy-Optimal Unmanned Aerial Vehicles Motion Planning and Control Based on Integrated System Physical Dynamics
> Journal of Dynamic Systems, Measurement, and Control
Published Online: January 13, 2023
Fig. 9 Left: octorotor testing vehicle and right: UAV testing at Woodland-Davis Aeromodelers test site More
Image
in Energy-Optimal Unmanned Aerial Vehicles Motion Planning and Control Based on Integrated System Physical Dynamics
> Journal of Dynamic Systems, Measurement, and Control
Published Online: January 13, 2023
Fig. 10 Evolution of vehicle states in 50 m forward flight using optimized-trajectory-following and high-velocity baseline controllers: X -axis (forward) position for ( a ) OTF and ( b ) HVB, pitch angle for ( c ) OTF and ( d ) HVB, and power consumption for ( e ) OTF and ( f ) HVB More
Journal Articles
Article Type: Research-Article
J. Dyn. Sys., Meas., Control. April 2023, 145(4): 041001.
Paper No: DS-22-1091
Published Online: January 11, 2023
Image
in Self-Triggered Model Predictive Control With Sample-and-Hold Fashion for Constrained Continuous-Time Linear Systems
> Journal of Dynamic Systems, Measurement, and Control
Published Online: January 11, 2023
Fig. 1 The relationship between optimal predictive control signal and actual control signal More
Image
in Self-Triggered Model Predictive Control With Sample-and-Hold Fashion for Constrained Continuous-Time Linear Systems
> Journal of Dynamic Systems, Measurement, and Control
Published Online: January 11, 2023
Fig. 2 The relation of feasible control law More
Image
in Self-Triggered Model Predictive Control With Sample-and-Hold Fashion for Constrained Continuous-Time Linear Systems
> Journal of Dynamic Systems, Measurement, and Control
Published Online: January 11, 2023
Fig. 3 Sample-and-hold fashion with i samples More
Image
in Self-Triggered Model Predictive Control With Sample-and-Hold Fashion for Constrained Continuous-Time Linear Systems
> Journal of Dynamic Systems, Measurement, and Control
Published Online: January 11, 2023
Fig. 4 The state trajectories x 1 ( t ) under three cases More