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Nonlinear programming control using differential aerodynamic drag for CubeSat formation flying Article

Sheng-chao DENG, Tao MENG, Zhong-he JIN

Frontiers of Information Technology & Electronic Engineering 2017, Volume 18, Issue 7,   Pages 867-881 doi: 10.1631/FITEE.1500493

Abstract: achieve the desired in-track formation through the atmospheric drag difference, which will be used on ZJUCubeSatNumerical simulation based on ZJUCubeSat verifies the feasibility and advantage of this design.

Keywords： QB50     ZJUCubeSat     Atmospheric drag     Formation flying    

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Nonlinear programming control using differential aerodynamic drag for CubeSat formation flying

Sheng-chao DENG, Tao MENG, Zhong-he JIN

Journal Article