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You searched for +publisher:"York University" +contributor:("Zhu, George"). Showing records 1 – 9 of 9 total matches.

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York University

1. Dong, Gangqi. Autonomous Visual Servo Robotic Capture of Non-cooperative Target.

Degree: PhD, Earth & Space Science, 2017, York University

 This doctoral research develops and validates experimentally a vision-based control scheme for the autonomous capture of a non-cooperative target by robotic manipulators for active space… (more)

Subjects/Keywords: Engineering; Robotic manipulator; Visual servo; Non-cooperative target; Target estimation; Autonomous capture; Kinematics-based robotic control; Joint flexibility; On orbit servicing; Active debris removal

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APA (6th Edition):

Dong, G. (2017). Autonomous Visual Servo Robotic Capture of Non-cooperative Target. (Doctoral Dissertation). York University. Retrieved from http://hdl.handle.net/10315/33406

Chicago Manual of Style (16th Edition):

Dong, Gangqi. “Autonomous Visual Servo Robotic Capture of Non-cooperative Target.” 2017. Doctoral Dissertation, York University. Accessed March 01, 2021. http://hdl.handle.net/10315/33406.

MLA Handbook (7th Edition):

Dong, Gangqi. “Autonomous Visual Servo Robotic Capture of Non-cooperative Target.” 2017. Web. 01 Mar 2021.

Vancouver:

Dong G. Autonomous Visual Servo Robotic Capture of Non-cooperative Target. [Internet] [Doctoral dissertation]. York University; 2017. [cited 2021 Mar 01]. Available from: http://hdl.handle.net/10315/33406.

Council of Science Editors:

Dong G. Autonomous Visual Servo Robotic Capture of Non-cooperative Target. [Doctoral Dissertation]. York University; 2017. Available from: http://hdl.handle.net/10315/33406


York University

2. Agarwal, Anirudh. Proportional-Derivative-Acceleration Feedback Controller Design for Single Axis Attitude Control of Rigid Spacecraft with Flexible Appendages.

Degree: MSc -MS, Earth & Space Science, 2019, York University

 This study designs and analyzes a new type of controller that helps improve the performance of single axis attitude control of flexible appendages attached to… (more)

Subjects/Keywords: Aerospace engineering; Spacecraft dynamics; Control systems; Acceleration feedback; PIDA; PID; Attitude control; Classical control; Spacecraft attitude control; Single axis attitude control

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APA (6th Edition):

Agarwal, A. (2019). Proportional-Derivative-Acceleration Feedback Controller Design for Single Axis Attitude Control of Rigid Spacecraft with Flexible Appendages. (Masters Thesis). York University. Retrieved from http://hdl.handle.net/10315/35911

Chicago Manual of Style (16th Edition):

Agarwal, Anirudh. “Proportional-Derivative-Acceleration Feedback Controller Design for Single Axis Attitude Control of Rigid Spacecraft with Flexible Appendages.” 2019. Masters Thesis, York University. Accessed March 01, 2021. http://hdl.handle.net/10315/35911.

MLA Handbook (7th Edition):

Agarwal, Anirudh. “Proportional-Derivative-Acceleration Feedback Controller Design for Single Axis Attitude Control of Rigid Spacecraft with Flexible Appendages.” 2019. Web. 01 Mar 2021.

Vancouver:

Agarwal A. Proportional-Derivative-Acceleration Feedback Controller Design for Single Axis Attitude Control of Rigid Spacecraft with Flexible Appendages. [Internet] [Masters thesis]. York University; 2019. [cited 2021 Mar 01]. Available from: http://hdl.handle.net/10315/35911.

Council of Science Editors:

Agarwal A. Proportional-Derivative-Acceleration Feedback Controller Design for Single Axis Attitude Control of Rigid Spacecraft with Flexible Appendages. [Masters Thesis]. York University; 2019. Available from: http://hdl.handle.net/10315/35911


York University

3. Li, Peng. Dynamics and Control of Spacecraft Rendezvous By Nonlinear Model Predictive Control.

Degree: PhD, Earth & Space Science, 2019, York University

 This doctoral research investigates the fundamental problems in the dynamics and control of spacecraft rendezvous with a non-cooperative tumbling target. New control schemes based on… (more)

Subjects/Keywords: Aerospace engineering; Spacecraft Rendezvous; Proximity Operation; Autonomous Rendezvous; Nonlinear Model Predictive Control

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APA (6th Edition):

Li, P. (2019). Dynamics and Control of Spacecraft Rendezvous By Nonlinear Model Predictive Control. (Doctoral Dissertation). York University. Retrieved from http://hdl.handle.net/10315/35890

Chicago Manual of Style (16th Edition):

Li, Peng. “Dynamics and Control of Spacecraft Rendezvous By Nonlinear Model Predictive Control.” 2019. Doctoral Dissertation, York University. Accessed March 01, 2021. http://hdl.handle.net/10315/35890.

MLA Handbook (7th Edition):

Li, Peng. “Dynamics and Control of Spacecraft Rendezvous By Nonlinear Model Predictive Control.” 2019. Web. 01 Mar 2021.

Vancouver:

Li P. Dynamics and Control of Spacecraft Rendezvous By Nonlinear Model Predictive Control. [Internet] [Doctoral dissertation]. York University; 2019. [cited 2021 Mar 01]. Available from: http://hdl.handle.net/10315/35890.

Council of Science Editors:

Li P. Dynamics and Control of Spacecraft Rendezvous By Nonlinear Model Predictive Control. [Doctoral Dissertation]. York University; 2019. Available from: http://hdl.handle.net/10315/35890


York University

4. Sidhu, Gurtej Singh. Fabrication and Characterization of Self-Sensing Nanocomposite - "Smart Skin".

Degree: MASc - Master of Applied Science, Mechanical Engineering, 2019, York University

 This study characterizes the behaviour and properties of self-sensing polymer nanocomposite. Specifically, we studied the Electrical, Mechanical and Piezoresistive properties. Electrically the material is conductive… (more)

Subjects/Keywords: Nanotechnology; self sensing; smart material; nanocomposite; strain sensor; smart sensor; multifunctional; piezoresistive sensor; carbon nanotubes; Polydimethylsiloxane; PDMS; MWCNT

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APA (6th Edition):

Sidhu, G. S. (2019). Fabrication and Characterization of Self-Sensing Nanocomposite - "Smart Skin". (Masters Thesis). York University. Retrieved from http://hdl.handle.net/10315/35896

Chicago Manual of Style (16th Edition):

Sidhu, Gurtej Singh. “Fabrication and Characterization of Self-Sensing Nanocomposite - "Smart Skin".” 2019. Masters Thesis, York University. Accessed March 01, 2021. http://hdl.handle.net/10315/35896.

MLA Handbook (7th Edition):

Sidhu, Gurtej Singh. “Fabrication and Characterization of Self-Sensing Nanocomposite - "Smart Skin".” 2019. Web. 01 Mar 2021.

Vancouver:

Sidhu GS. Fabrication and Characterization of Self-Sensing Nanocomposite - "Smart Skin". [Internet] [Masters thesis]. York University; 2019. [cited 2021 Mar 01]. Available from: http://hdl.handle.net/10315/35896.

Council of Science Editors:

Sidhu GS. Fabrication and Characterization of Self-Sensing Nanocomposite - "Smart Skin". [Masters Thesis]. York University; 2019. Available from: http://hdl.handle.net/10315/35896


York University

5. Li, Gangqiang. Multibody Dynamics and Control of Tethered Spacecraft Systems.

Degree: PhD, Earth & Space Science, 2019, York University

 This doctoral research conducts high-fidelity multiphysics modeling for tethered spacecraft systems, such as electrodynamic tether systems, electric solar wind sail systems, and tether transportation systems… (more)

Subjects/Keywords: Computer engineering; Finite element method; Tethered spacecraft systems; Control; Dynamics; Electric solar wind sail; Tether transportation system; Partial space elevator; Space elevator; Electrodynamic tether systems

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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6th Edition):

Li, G. (2019). Multibody Dynamics and Control of Tethered Spacecraft Systems. (Doctoral Dissertation). York University. Retrieved from https://yorkspace.library.yorku.ca/xmlui/handle/10315/36739

Chicago Manual of Style (16th Edition):

Li, Gangqiang. “Multibody Dynamics and Control of Tethered Spacecraft Systems.” 2019. Doctoral Dissertation, York University. Accessed March 01, 2021. https://yorkspace.library.yorku.ca/xmlui/handle/10315/36739.

MLA Handbook (7th Edition):

Li, Gangqiang. “Multibody Dynamics and Control of Tethered Spacecraft Systems.” 2019. Web. 01 Mar 2021.

Vancouver:

Li G. Multibody Dynamics and Control of Tethered Spacecraft Systems. [Internet] [Doctoral dissertation]. York University; 2019. [cited 2021 Mar 01]. Available from: https://yorkspace.library.yorku.ca/xmlui/handle/10315/36739.

Council of Science Editors:

Li G. Multibody Dynamics and Control of Tethered Spacecraft Systems. [Doctoral Dissertation]. York University; 2019. Available from: https://yorkspace.library.yorku.ca/xmlui/handle/10315/36739


York University

6. Santaguida, Lucas Francesco. Study of Autonomous Capture and Detumble of Non-Cooperative Target by a Free-Flying Space Manipulator Using an Air-Bearing Platform.

Degree: MASc - Master of Applied Science, Mechanical Engineering, 2020, York University

 This thesis developed a 3-DOF satellite simulator with an attached 3-DOF manipulator to capture and detumble a target satellite simulator. Existing systems are heavily dependent… (more)

Subjects/Keywords: Robotics; On-Orbit Servicing; Air-bearing testbed; Planning; Space Vehicles; Autonomous; Free-Flying Space Robotic; Orbital Robotics

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APA (6th Edition):

Santaguida, L. F. (2020). Study of Autonomous Capture and Detumble of Non-Cooperative Target by a Free-Flying Space Manipulator Using an Air-Bearing Platform. (Masters Thesis). York University. Retrieved from http://hdl.handle.net/10315/37778

Chicago Manual of Style (16th Edition):

Santaguida, Lucas Francesco. “Study of Autonomous Capture and Detumble of Non-Cooperative Target by a Free-Flying Space Manipulator Using an Air-Bearing Platform.” 2020. Masters Thesis, York University. Accessed March 01, 2021. http://hdl.handle.net/10315/37778.

MLA Handbook (7th Edition):

Santaguida, Lucas Francesco. “Study of Autonomous Capture and Detumble of Non-Cooperative Target by a Free-Flying Space Manipulator Using an Air-Bearing Platform.” 2020. Web. 01 Mar 2021.

Vancouver:

Santaguida LF. Study of Autonomous Capture and Detumble of Non-Cooperative Target by a Free-Flying Space Manipulator Using an Air-Bearing Platform. [Internet] [Masters thesis]. York University; 2020. [cited 2021 Mar 01]. Available from: http://hdl.handle.net/10315/37778.

Council of Science Editors:

Santaguida LF. Study of Autonomous Capture and Detumble of Non-Cooperative Target by a Free-Flying Space Manipulator Using an Air-Bearing Platform. [Masters Thesis]. York University; 2020. Available from: http://hdl.handle.net/10315/37778


York University

7. Cookson, Joshua Jonathan. Experimental Investigation of Spacecraft Rendezvous and Docking by Development of a 3 Degree of Freedom Satellite Simulator Testbed.

Degree: MSc -MS, Earth & Space Science, 2020, York University

 This thesis developed a 3 degree of freedom air bearing satellite simulator testbed. The major components of this testbed are a 2-meter by 4-meter granite… (more)

Subjects/Keywords: Aerospace engineering; Planar; Air bearing; Satellite; Test bed; 3DOF; Spacecraft; Dynamics; Docking; Satellite simulator

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APA (6th Edition):

Cookson, J. J. (2020). Experimental Investigation of Spacecraft Rendezvous and Docking by Development of a 3 Degree of Freedom Satellite Simulator Testbed. (Masters Thesis). York University. Retrieved from https://yorkspace.library.yorku.ca/xmlui/handle/10315/37388

Chicago Manual of Style (16th Edition):

Cookson, Joshua Jonathan. “Experimental Investigation of Spacecraft Rendezvous and Docking by Development of a 3 Degree of Freedom Satellite Simulator Testbed.” 2020. Masters Thesis, York University. Accessed March 01, 2021. https://yorkspace.library.yorku.ca/xmlui/handle/10315/37388.

MLA Handbook (7th Edition):

Cookson, Joshua Jonathan. “Experimental Investigation of Spacecraft Rendezvous and Docking by Development of a 3 Degree of Freedom Satellite Simulator Testbed.” 2020. Web. 01 Mar 2021.

Vancouver:

Cookson JJ. Experimental Investigation of Spacecraft Rendezvous and Docking by Development of a 3 Degree of Freedom Satellite Simulator Testbed. [Internet] [Masters thesis]. York University; 2020. [cited 2021 Mar 01]. Available from: https://yorkspace.library.yorku.ca/xmlui/handle/10315/37388.

Council of Science Editors:

Cookson JJ. Experimental Investigation of Spacecraft Rendezvous and Docking by Development of a 3 Degree of Freedom Satellite Simulator Testbed. [Masters Thesis]. York University; 2020. Available from: https://yorkspace.library.yorku.ca/xmlui/handle/10315/37388


York University

8. Li, Gangqiang. Multibody Dynamics and Control of Tethered Spacecraft Systems.

Degree: PhD, Earth & Space Science, 2019, York University

 This doctoral research conducts high-fidelity multiphysics modeling for tethered spacecraft systems, such as electrodynamic tether systems, electric solar wind sail systems, and tether transportation systems… (more)

Subjects/Keywords: Computer engineering; Finite element method; Tethered spacecraft systems; Control; Dynamics; Electric solar wind sail; Tether transportation system; Partial space elevator; Space elevator; Electrodynamic tether systems

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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6th Edition):

Li, G. (2019). Multibody Dynamics and Control of Tethered Spacecraft Systems. (Doctoral Dissertation). York University. Retrieved from http://hdl.handle.net/10315/36739

Chicago Manual of Style (16th Edition):

Li, Gangqiang. “Multibody Dynamics and Control of Tethered Spacecraft Systems.” 2019. Doctoral Dissertation, York University. Accessed March 01, 2021. http://hdl.handle.net/10315/36739.

MLA Handbook (7th Edition):

Li, Gangqiang. “Multibody Dynamics and Control of Tethered Spacecraft Systems.” 2019. Web. 01 Mar 2021.

Vancouver:

Li G. Multibody Dynamics and Control of Tethered Spacecraft Systems. [Internet] [Doctoral dissertation]. York University; 2019. [cited 2021 Mar 01]. Available from: http://hdl.handle.net/10315/36739.

Council of Science Editors:

Li G. Multibody Dynamics and Control of Tethered Spacecraft Systems. [Doctoral Dissertation]. York University; 2019. Available from: http://hdl.handle.net/10315/36739


York University

9. Furtal, Jude Joseph. Structural Design and Finite Element Analysis of DESCENT CubeSats.

Degree: MASc - Master of Applied Science, Mechanical Engineering, 2020, York University

 This thesis outlines the development of a two custom CubeSat structures used for the DESCENT mission. DESCENT aims to test the feasibility of Electrodynamic Tethers… (more)

Subjects/Keywords: Aerospace engineering; Satellites; Cubesats; Finite element analysis; Structural design; Mechanical design

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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6th Edition):

Furtal, J. J. (2020). Structural Design and Finite Element Analysis of DESCENT CubeSats. (Masters Thesis). York University. Retrieved from https://yorkspace.library.yorku.ca/xmlui/handle/10315/37381

Chicago Manual of Style (16th Edition):

Furtal, Jude Joseph. “Structural Design and Finite Element Analysis of DESCENT CubeSats.” 2020. Masters Thesis, York University. Accessed March 01, 2021. https://yorkspace.library.yorku.ca/xmlui/handle/10315/37381.

MLA Handbook (7th Edition):

Furtal, Jude Joseph. “Structural Design and Finite Element Analysis of DESCENT CubeSats.” 2020. Web. 01 Mar 2021.

Vancouver:

Furtal JJ. Structural Design and Finite Element Analysis of DESCENT CubeSats. [Internet] [Masters thesis]. York University; 2020. [cited 2021 Mar 01]. Available from: https://yorkspace.library.yorku.ca/xmlui/handle/10315/37381.

Council of Science Editors:

Furtal JJ. Structural Design and Finite Element Analysis of DESCENT CubeSats. [Masters Thesis]. York University; 2020. Available from: https://yorkspace.library.yorku.ca/xmlui/handle/10315/37381

.