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On the nodal distance between two Keplerian trajectories with a common focus

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Abstract

We study the possible values of the nodal distance \(\delta _\mathrm{nod}\) between two non-coplanar Keplerian trajectories \(\mathcal{A}, \mathcal{A}'\) with a common focus. In particular, given \(\mathcal{A}'\) and assuming it is bounded, we compute optimal lower and upper bounds for \(\delta _\mathrm{nod}\) as functions of a selected pair of orbital elements of \(\mathcal{A}\), when the other elements can vary. This work arises in the attempt to extend to the elliptic case the optimal estimates for the orbit distance given in Gronchi and Valsecchi (Mon Not R Astron Soc 29(3):2687–2699, 2013) in case of a circular trajectory \(\mathcal{A}'\). These estimates are relevant to understand the observability of celestial bodies moving (approximately) along \(\mathcal{A}\) when the observer trajectory is (close to) \(\mathcal{A}'\).

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Notes

  1. Minimal Orbital Intersection Distance.

  2. Defined by assigning an orientation to both trajectories.

  3. \((I,\Omega ,\omega )\) and \((I',\Omega ',\omega ')\) are, respectively, inclination, longitude of the ascending node, argument of pericenter of \(\mathcal{A}\) and \(\mathcal{A}'\).

  4. We admit infinite values for the considered functions, e.g., \(\ell ^\omega _\mathrm{int}(q,0) = -\,\infty \).

  5. Here \(\ell ^{\,e}_\mathrm{int}(q,1)=-\,\infty \), and \(u^{\,e}_\mathrm{link}(q,1)=Q'-q\).

  6. Here we state the result presented in Gronchi and Valsecchi (2013) with a formula that is not singular for \(e=1\).

  7. We discard the solution giving a value of \(\xi '\) which is \(<-1\).

  8. We discard the solution giving a negative value of e.

  9. https://newton.spacedys.com/neodys.

References

  • Casanova, D., Tardioli, C., Lemaître, A.: Space debris collision avoidance using a three-filter sequence. Mon. Not. R. Astron. Soc. 442, 3235–3242 (2014)

    Article  ADS  Google Scholar 

  • Farnocchia, D., Chesley, S.R., Milani, A., Gronchi, G.F., Chodas, P.W.: Orbits, long-term prodictions, and impact monitoring. In: Michel, P., DeMeo, F.E., Bottke, W.F. (eds.) Asteroids IV. University of Arizona, Tucson (2016)

    Google Scholar 

  • Farnocchia, D., Eggl, S., Chodas, P.W., Giorgini, J.D., Chesley, S.R.: Planetary encounter analysis on the B-plane: a comprehensive formulation. Celest. Mech. Dyn. Astron. 131(8), 36 (2019)

    Article  ADS  MathSciNet  Google Scholar 

  • Gronchi, G.F.: On the stationary points of the squared distance between two ellipses with a common focus. SIAM J. Sci. Comput. 24(1), 61–80 (2002)

    Article  MathSciNet  Google Scholar 

  • Gronchi, G.F.: An algebraic method to compute the critical points of the distance function between two Keplerian orbits. Celest. Mech. Dyn. Astron. 93(1), 297–332 (2005)

    ADS  MathSciNet  MATH  Google Scholar 

  • Gronchi, G.F., Valsecchi, G.B.: On the possible values of the orbit distance between a near-Earth asteroid and the Earth. Mon. Not. R. Astron. Soc. 429(3), 2687–2699 (2013)

    Article  ADS  Google Scholar 

  • Hoots, F.R., Crawford, L.L., Roehrich, R.L.: An analytic method to determine future close approaches between satellites. Celest. Mech. 33(2), 143–158 (1984)

    Article  ADS  Google Scholar 

  • Kholshevnikov, K.V., Vassiliev, N.N.: On linking coefficient of two Keplerian orbits. Celest. Mech. Dyn. Astron. 75(1), 67–74 (1999a)

    Article  ADS  MathSciNet  Google Scholar 

  • Kholshevnikov, K.V., Vassiliev, N.N.: On the distance function between two Keplerian elliptic orbits. Celest. Mech. Dyn. Astron. 75(2), 75–83 (1999b)

    Article  ADS  MathSciNet  Google Scholar 

  • Mikryukov, D.V., Baluev, R.V.: A lower bound of the distance between two elliptic orbits. Celest. Mech. Dyn. Astron. 131(6), 28 (2019)

    Article  ADS  MathSciNet  Google Scholar 

  • Milani, A.: Asteroid impact monitoring. Serb. Astron. J. 172, 1–11 (2006)

    Article  ADS  Google Scholar 

  • Sitarski, G.: Approaches of the parabolic comets to the outer planets. Acta Astron. 18(2), 171–195 (1968)

    ADS  Google Scholar 

Download references

Acknowledgements

Part of this work has been done during a visiting period of G. F. Gronchi at the Institut de mécanique céleste et de calcul des éphémérides (IMCCE), Observatoire de Paris. The same author also acknowledges the Project MIUR-PRIN 20178CJA2B titled “New frontiers of Celestial Mechanics: theory and applications”. We thank the anonymous referees for their suggestions, allowing us to improve the paper.

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Correspondence to Giovanni Federico Gronchi.

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Gronchi, G.F., Niederman, L. On the nodal distance between two Keplerian trajectories with a common focus. Celest Mech Dyn Astr 132, 5 (2020). https://doi.org/10.1007/s10569-019-9944-y

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