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Journal Articles
Publisher: ASME
Article Type: Research Papers
Letters Dyn. Sys. Control. April 2025, 5(2): 021004.
Paper No: ALDSC-24-1039
Published Online: November 25, 2024
Image
in Optimal Periodic Impulsive Control for Orbital Stabilization of Underactuated Systems
> ASME Letters in Dynamic Systems and Control
Published Online: November 25, 2024
Fig. 1 Schematic diagram of Pendubot More about this image found in Schematic diagram of Pendubot
Image
in Optimal Periodic Impulsive Control for Orbital Stabilization of Underactuated Systems
> ASME Letters in Dynamic Systems and Control
Published Online: November 25, 2024
Fig. 2 Phase portrait of the Pendubot orbit O d More about this image found in Phase portrait of the Pendubot orbit O d
Image
in Optimal Periodic Impulsive Control for Orbital Stabilization of Underactuated Systems
> ASME Letters in Dynamic Systems and Control
Published Online: November 25, 2024
Fig. 3 Simulation results for p = 1 without parameter uncertainty More about this image found in Simulation results for p = 1 without parameter uncertainty
Image
in Optimal Periodic Impulsive Control for Orbital Stabilization of Underactuated Systems
> ASME Letters in Dynamic Systems and Control
Published Online: November 25, 2024
Fig. 4 Simulation results for p = 1 with parameter uncertainty More about this image found in Simulation results for p = 1 with parameter uncertainty
Image
in Optimal Periodic Impulsive Control for Orbital Stabilization of Underactuated Systems
> ASME Letters in Dynamic Systems and Control
Published Online: November 25, 2024
Fig. 5 Simulation results for p = 6 with parameter uncertainty More about this image found in Simulation results for p = 6 with parameter uncertainty
Image
in Optimal Periodic Impulsive Control for Orbital Stabilization of Underactuated Systems
> ASME Letters in Dynamic Systems and Control
Published Online: November 25, 2024
Fig. 6 Simulation results for p = 6 with parameter uncertainty. The gain of the terminal weighting matrix used was five times higher than the value in Eq. (26) , the results of which are presented in Fig. 5 . More about this image found in Simulation results for p = 6 with parameter uncertainty. The gain o...
Journal Articles
Publisher: ASME
Article Type: Editorial
Letters Dyn. Sys. Control. January 2025, 5(1): 010201.
Paper No: ALDSC-24-1055
Published Online: November 22, 2024
Journal Articles
Accepted Manuscript
Publisher: ASME
Article Type: Research Papers
Letters Dyn. Sys. Control.
Paper No: ALDSC-24-1016
Published Online: November 18, 2024
Journal Articles
Publisher: ASME
Article Type: Research Papers
Letters Dyn. Sys. Control. April 2025, 5(2): 021003.
Paper No: ALDSC-24-1009
Published Online: November 6, 2024
Journal Articles
Publisher: ASME
Article Type: Technical Briefs
Letters Dyn. Sys. Control. April 2025, 5(2): 024501.
Paper No: ALDSC-24-1025
Published Online: November 6, 2024
Image
in Minimum-Time Control of a Linear System With Input Saturation: A Practical Approach
> ASME Letters in Dynamic Systems and Control
Published Online: November 6, 2024
Fig. 1 Near-minimum-time control algorithm for a double integrator system More about this image found in Near-minimum-time control algorithm for a double integrator system
Image
in Minimum-Time Control of a Linear System With Input Saturation: A Practical Approach
> ASME Letters in Dynamic Systems and Control
Published Online: November 6, 2024
Fig. 2 True optimal control input via the new algorithm for triple integrator system ( x ( 0 ) = − [ 1 0 0 ] T ) More about this image found in True optimal control input via the new algorithm for triple integrator syst...
Image
in Minimum-Time Control of a Linear System With Input Saturation: A Practical Approach
> ASME Letters in Dynamic Systems and Control
Published Online: November 6, 2024
Fig. 3 Control input for non-optimal sampling period (triple integrator system, h = 1 s, x ( 0 ) = − [ 1 0 0 ] T ) More about this image found in Control input for non-optimal sampling period (triple integrator system, h...
Image
in Minimum-Time Control of a Linear System With Input Saturation: A Practical Approach
> ASME Letters in Dynamic Systems and Control
Published Online: November 6, 2024
Fig. 4 Control input for non-optimal sampling period (triple integrator system, h = 0.8 s, x ( 0 ) = − [ 1 0 0 ] T ) More about this image found in Control input for non-optimal sampling period (triple integrator system, h...
Image
in Minimum-Time Control of a Linear System With Input Saturation: A Practical Approach
> ASME Letters in Dynamic Systems and Control
Published Online: November 6, 2024
Fig. 5 Near-minimum-time control input via the new algorithm for triple integrator system ( x ( 0 ) = − [ 1 − 1 1 ] T ) More about this image found in Near-minimum-time control input via the new algorithm for triple integrator...
Image
in Minimum-Time Control of a Linear System With Input Saturation: A Practical Approach
> ASME Letters in Dynamic Systems and Control
Published Online: November 6, 2024
Fig. 6 States for triple integrator system ( x ( 0 ) = − [ 1 − 1 1 ] T ) More about this image found in States for triple integrator system ( x ( 0 ) = − [ 1 ...
Image
in Minimum-Time Control of a Linear System With Input Saturation: A Practical Approach
> ASME Letters in Dynamic Systems and Control
Published Online: November 6, 2024
Fig. 7 Near-minimum-time control input via new algorithm for rigid-flexible system ( ζ 1 = 0 , n m = 1 ) More about this image found in Near-minimum-time control input via new algorithm for rigid-flexible system...
Image
in Minimum-Time Control of a Linear System With Input Saturation: A Practical Approach
> ASME Letters in Dynamic Systems and Control
Published Online: November 6, 2024
Fig. 8 Near-minimum-time control input via new algorithm for unstable rigid-flexible system ( h = 1.14 s, ζ 1 = − 0.2 , n m = 1 ) More about this image found in Near-minimum-time control input via new algorithm for unstable rigid-flexib...
Image
in Minimum-Time Control of a Linear System With Input Saturation: A Practical Approach
> ASME Letters in Dynamic Systems and Control
Published Online: November 6, 2024
Fig. 9 Rigid mode states ( h = 1.14 s, ζ 1 = − 0.2 , n m = 1 ) More about this image found in Rigid mode states ( h = 1.14 s, ζ 1 = − 0.2 , n m = 1 ...
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