Simo, Jules and McInnes, Colin (2012) Feedback stabilization of displaced periodic orbits : Application to binary asteroid. In: 22nd AAS/AIAA Spaceflight Mechanics Meeting, 2012-01-29 - 2012-02-02, Charleston, South Carolina.
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This paper investigates displaced periodic orbits at linear order in the circular restricted Earth-Moon system (CRTBP), where the third massless body utilizes a hybrid of solar sail and a solar electric propulsion (SEP). A feedback linearization control scheme is implemented to perform stabilization and trajectory tracking for the nonlinear system. Attention is now directed to binary asteroid systems as an application of the restricted problem. The idea of combining a solar sail with an SEP auxiliary system to obtain a hybrid sail system is important especially due to the challenges of performing complex trajectories.
|Item type:||Conference or Workshop Item (Paper)|
|Keywords:||periodic orbits, circular restricted Earth-Moon system (CRTBP) , solar electric propulsion (SEP) , solar sail, trajectory tracking , binary asteroid systems , hybrid sail system, Mechanical engineering and machinery, Motor vehicles. Aeronautics. Astronautics, Mechanical Engineering, Aerospace Engineering, Control and Systems Engineering|
|Subjects:||Technology > Mechanical engineering and machinery|
Technology > Motor vehicles. Aeronautics. Astronautics
|Department:||Faculty of Engineering > Mechanical and Aerospace Engineering|
Technology and Innovation Centre > Advanced Engineering and Manufacturing
|Depositing user:||Pure Administrator|
|Date Deposited:||18 Jan 2012 11:26|
|Last modified:||02 Jul 2014 07:29|
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