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FLY-BY ME TO THE MOON
LESSONS LEARNED ON CLOSE ENCOUNTERS
Ettore Perozzi
Deimos Space
[email protected]
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FLY-BY ME TO THE MOON: LESSONS LEARNED ON CLOSE ENCOUNTERS
E. Perozzi, Deimos Space
Heidelberg 1984
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FLY-BY ME TO THE MOON: LESSONS LEARNED ON CLOSE ENCOUNTERS
E. Perozzi, Deimos Space
GRAVITY ASSIST
Guido Von Pirquet : Voyages to the Planets, (Die
Rakete, 1928)
Michael Minovitch : A Method for Determining
Interplanetary Free-Fall Reconnaissance Trajectories
(JPL TR 312-130, 1961)
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FLY-BY ME TO THE MOON: LESSONS LEARNED ON CLOSE ENCOUNTERS
E. Perozzi, Deimos Space
CASSINI MISSION ANALYSIS
Perozzi, E. (1986) Cassini Mission: Dynamics of the Titan close encounter. In proc. The Solid Bodies of the Outer
Solar System, A. Coradini and M. Fulchignoni eds, ESA SP-242
Greenberg, R., Carusi, A., Valsecchi, G.B. , (1988) Outcomes of Planetary Close Encounters : A Systematic
Comparison of Methodologies. Icarus 75
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FLY-BY ME TO THE MOON: LESSONS LEARNED ON CLOSE ENCOUNTERS
E. Perozzi, Deimos Space
B-PLANE TARGETING
Perozzi, E. (1986) Cassini Mission: Dynamics of the Titan close encounter. In proc. The Solid Bodies of the Outer
Solar System, A. Coradini and M. Fulchignoni eds, ESA SP-242
Greenberg, R., Carusi, A., Valsecchi, G.B. , (1988) Outcomes of Planetary Close Encounters : A Systematic
Comparison of Methodologies. Icarus 75
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FLY-BY ME TO THE MOON: LESSONS LEARNED ON CLOSE ENCOUNTERS
E. Perozzi, Deimos Space
DYNAMICS OF COMETS
Carusi, A., Valsecchi, G.B., Kresak, L. (1982) Orbital patterns of interplanetary objects at close
encounters with Jupiter. Bulletin of the Astronomical Institutes of Czechoslovakia 33,141.
Broucke, R.A.: On the History of the Slingshot Effect and Cometary Orbits. AAS 01-435 .(2001)
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FLY-BY ME TO THE MOON: LESSONS LEARNED ON CLOSE ENCOUNTERS
E. Perozzi, Deimos Space
THE TISSERAND INVARIANT
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T   2 a (1  e 2 ) cos i
a
U  3T
The Tisserand Invariant is a reduced form of the Jacobi Integral related
to the unperturbed relative velocity U at encounter
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FLY-BY ME TO THE MOON: LESSONS LEARNED ON CLOSE ENCOUNTERS
E. Perozzi, Deimos Space
LUNAR BALLISTIC CAPTURE
Belbruno, E.A. and Miller, J.K. (1990) A ballistic lunar capture trajectory
for the Japanese spacecraft Hiten. JPL report IOM 312/90.4-1317.
Howell, K.C., Marchand, B.G., Lo, M.W. (2001) Temporary satellite
capture of short-period Jupiter family comets from the perspective of
dynamical systems. Journal of the Astronautical Sciences 49(4).
LUNAR ORBIT
LUNAR ORBIT
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FLY-BY ME TO THE MOON: LESSONS LEARNED ON CLOSE ENCOUNTERS
E. Perozzi, Deimos Space
SPACE MANIFOLD DYNAMICS
LL
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L1 FUZZY BOUNDARY
STABLE MANIFOLD
Ross, S.D., Scheeres, D.J. (2007) Multiple Gravity Assists, Capture, and Escape in the Restricted Three-Body
Problem. SIAM Journal on Applied Dynamical Systems 6(3).
Belló, M., Gómez, G., Masdemont, G.G. (2009) Invariant manifolds, Lagrangian trajectories and space mission
design. In Space Manifold Dynamics. E. Perozzi and S. Ferraz-Mello eds, Springer New York.
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FLY-BY ME TO THE MOON: LESSONS LEARNED ON CLOSE ENCOUNTERS
E. Perozzi, Deimos Space
SPACE MANIFOLD DYNAMICS
E. Perozzi and S. Ferraz-Mello
(eds): Space Manifold Dynamics.
Springer USA, 2010.
Campagnola, S., Skerritt, P., Russell, R.P. (2012) Flybys in the
planar, circular, restricted, three-body problem. Celestial Mechanics
& Dynamical Astronomy.
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FLY-BY ME TO THE MOON: LESSONS LEARNED ON CLOSE ENCOUNTERS
E. Perozzi, Deimos Space
one cannot predict how knowledge will be applied
only that it often is
(Charles Conley, 1968)
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