Bounded relative motion under zonal harmonics perturbations

The problem of finding natural bounded relative trajectories between the different units of a distributed space system is of great interest to the astrodynamics community. This is because most popular initialization methods still fail to establish long-term bounded relative motion when gravitational perturbations are involved. Recent numerical searches based on dynamical systems theory and ergodic maps have demonstrated that bounded relative trajectories not only exist but may extend up to hundreds of kilometers, i.e., well beyond the reach of currently available techniques. To remedy this, we introduce a novel approach that relies on neither linearized equations nor mean-to-osculating orbit element mappings. The proposed algorithm applies to rotationally symmetric bodies and is based on a numerical method for computing quasi-periodic invariant tori via stroboscopic maps, including extra constraints to fix the average of the nodal period and RAAN drift between two consecutive equatorial plane crossings of the quasi-periodic solutions. In this way, bounded relative trajectories of arbitrary size can be found with great accuracy as long as these are allowed by the natural dynamics and the physical constraints of the system (e.g., the surface of the gravitational attractor). This holds under any number of zonal harmonics perturbations and for arbitrary time intervals as demonstrated by numerical simulations about an Earth-like planet and the highly oblate primary of the binary asteroid (66391) 1999 KW4.

[1]  R. Broucke,et al.  Numerical integration of periodic orbits in the main problem of artificial satellite theory , 1994 .

[2]  M. Watkins,et al.  The gravity recovery and climate experiment: Mission overview and early results , 2004 .

[3]  G. Gómez,et al.  The dynamics around the collinear equilibrium points of the RTBP , 2001 .

[4]  Owen Brown,et al.  The Value Proposition for Fractionated Space Architectures , 2006 .

[5]  P. Gurfil Relative Motion between Elliptic Orbits: Generalized Boundedness Conditions and Optimal Formationkeeping , 2005 .

[6]  H. Schaub,et al.  J2 Invariant Relative Orbits for Spacecraft Formations , 2001 .

[7]  B. Tapley,et al.  Statistical Orbit Determination , 2004 .

[8]  V. Becerra,et al.  Using Newton's method to search for quasi-periodic relative satellite motion based on nonlinear Hamilton models , 2006 .

[9]  Daniel J. Scheeres,et al.  Bounded relative orbits about asteroids for formation flying and applications , 2016 .

[10]  Ming Xu,et al.  On the existence of J2 invariant relative orbits from the dynamical system point of view , 2012 .

[11]  Ming Xu,et al.  J2 invariant relative orbits via differential correction algorithm , 2007 .

[12]  Pini Gurfil,et al.  Solutions and periodicity of satellite relative motion under even zonal harmonics perturbations , 2011 .

[13]  Pini Gurfil,et al.  Multiple Poincaré sections method for finding the quasiperiodic orbits of the restricted three body problem , 2012 .

[14]  Dario Izzo,et al.  Special Inclinations Allowing Minimal Drift Orbits for Formation Flying Satellites , 2008 .

[15]  R. Seydel Practical Bifurcation and Stability Analysis , 1994 .

[16]  Gerhard Krieger,et al.  TanDEM-X: A radar interferometer with two formation-flying satellites , 2013 .

[17]  Daniel J. Scheeres,et al.  Radar Imaging of Binary Near-Earth Asteroid (66391) 1999 KW4 , 2006, Science.

[18]  Ben Breech,et al.  Transport of cross helicity and radial evolution of Alfvénicity in the solar wind , 2004 .

[19]  Jonathan P. How,et al.  Partial J2 Invariance for Spacecraft Formations , 2006 .

[20]  Dirk Brouwer,et al.  SOLUTION OF THE PROBLEM OF ARTIFICIAL SATELLITE THEORY WITHOUT DRAG , 1959 .

[21]  Jonathan P. How,et al.  Spacecraft Formation Flying: Dynamics, Control and Navigation , 2009 .

[22]  William M. Folkner,et al.  Alternative mission architectures for a gravity recovery satellite mission , 2009 .

[23]  Owen Brown,et al.  Fractionated Space Architectures: A Vision for Responsive Space , 2006 .

[24]  Jerrold E. Marsden,et al.  J2 DYNAMICS AND FORMATION FLIGHT , 2001 .

[25]  Srinivas R. Vadali,et al.  Fuel Optimal Control for Formation Flying of Satellites , 1999 .

[26]  M. D'Errico,et al.  Design of Satellite Formations for Interferometric and Bistatic SAR , 2007, 2007 IEEE Aerospace Conference.

[27]  D. Scheeres Orbital motion in strongly perturbed environments , 2012 .

[28]  P. Gurfil,et al.  The SAMSON Project – Cluster Flight and Geolocation with Three Autonomous Nano-satellites , 2012 .