Colombo, Camilla and Xu, Ming and McInnes, Colin (2012) Stabilisation of the hyperbolic equilibrium of high area-to-mass spacecraft. In: 63rd International Astronautical Congress, 2012-10-01 - 2012-10-05.
Colombo_C_et_al_Pure_Stabilisation_of_the_hyperbolic_equilibrium_of_high_area_to_mass_spacecraft_Oct_2012.pdf - Draft Version
In this paper we propose the exploitation of anti-heliotropic orbits, corresponding to the hyperbolic solution of the J2 and solar radiation pressure dynamical system, as gateway orbits between the low-eccentricity orbits where atmospheric drag does not affect the motion and the high eccentricity orbits which enter in drag regime. The eccentricity can be maintained in the neighborhood of the unstable point by means of a controller preserving the Hamiltonian structure of the system. In this way, any initial eccentricity close to the equilibrium conditions will lead to a bound trajectory around the controlled elliptic equilibrium. By selecting the time the controller is turned off, one of the two unstable manifolds leaving the equilibrium point can be followed, leading the orbit to become circular of to increase its eccentricity until natural decay occurs.
|Item type:||Conference or Workshop Item (Paper)|
|Keywords:||anti-heliotropic orbits , J2 , high area-to-mass spacecraft, solar radiation pressure, dynamical 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:||13 Sep 2012 15:04|
|Last modified:||28 Apr 2016 15:49|