Abstract
The theorem of mirror trajectories, proven almost six decades ago by Miele, states that for a given path in the restricted problem of three bodies (with primaries in mutual circular orbits) there exists a mirror trajectory (in two dimensions) and three mirror paths (in three dimensions). The theorem at hand regards feasible trajectories and proved extremely useful for investigating the spacecraft natural dynamics in the circular restricted problem of three bodies, by identifying special solutions, such as symmetric periodic orbits and free return paths. This theorem has recently been extended to optimal mirror trajectories, thus substantiating Miele’s conjecture based on numerical evidence. Unlike the theorem of mirror paths, which refers to natural (unpowered) orbital motion, the theorem of optimal mirror trajectories establishes the existence, characteristics, and optimal control time history of the returning path, once the outgoing optimal trajectory has been determined. This theorem applies to (i) finite-thrust trajectories, for which a limiting value of the thrust acceleration exists, (ii) constant-thrust-acceleration paths, (iii) impulsive trajectories, and (iv) artificial periodic orbits (that use very low thrust propulsion or solar sails). This work illustrates the theorem of optimal mirror trajectories applied to two cases of practical interest: (a) continuous, low-thrust orbit transfer, and (b) continuous-thrust lunar descent (with soft touchdown) and ascent (with final orbit injection). In both cases, the theorem allows the immediate and straightforward identification of the optimal control law of the returning path, once the outgoing optimal trajectory has been determined.
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References
R. Bellman, Dynamic Programming, Princeton University Press, Princeton, NJ, 1957
G. A. Bliss, Lectures on the Calculus of Variations, University of Chicago Press, Chicago, IL, pp. 108–112, 1946
A. E. Bryson and Y. C. Ho, Applied Optimal Control, Ginn and Company, Waltham, MA, 1969
P. Cicala, An Engineering Approach to the Calculus of Variations, Levrotto & Bella, Turin, Italy, 1957
W. Hohmann, “Die Erreichbarkeit der Himmelskoerper”, Oldenbourg, Munich, Germany, 1925; also “The Attainability of Heavenly Bodies”, NASA Translation TT-F-44, 1960
D. G. Hull, Optimal Control Theory for Applications, Springer, New York, 2003
D. F. Lawden, Optimal Trajectories for Space Navigation, Butterworths, London, U.K., 1963
G. Leitmann, “A calculus of variations solution of God-dard’s problem”, Astronautica Acta, Vol. 2, pp. 55–62, 1956
G. Leitmann (Ed.), Optimization Techniques, Academic Press, New York, NY, 1962
A. Miele, “General variational theory of the flight paths of Rocket-Powered aircraft, missiles, and satellite carriers”, Astronautica Acta, Vol. 4, pp. 11–21, 1958
A. Miele, “Theorem of Image Trajectories in Earth-Moon Space”, Astronautica Acta, Vol. 6, No. 5, pp. 225–232, 1960
A. Miele and S. Mancuso, “Optimal Trajectories for Earth-Moon-Earth Flight”, Acta Astronautica, Vol. 49, No. 2, pp. 59–71, 2001
A. Miele, “Revisit of the Theorem of Image Trajectories in Earth-Moon Space”, Journal of Optimization Theory and Applications, Vol. 147, No. 3, pp. 483–490, 2010
M. Pontani, P. Ghosh and B. A. Conway, “Particle Swarm Optimization of Multiple-Burn Rendezvous Trajectories”, Journal of Guidance, Control, and Dynamics, Vol. 35, No. 4, pp. 1192–1207, 2012
M. Pontani and B. A. Conway, “Particle Swarm Optimization Applied to Impulsive Orbital Transfers”, Acta Astro-nautica, Vol. 74, pp. 141–155, 2012
M. Pontani and B. A. Conway, “Optimal Finite-Thrust Rendezvous Trajectories Found via Particle Swarm Algorithm”, Journal of Spacecraft and Rockets, Vol. 50, pp. 1222–1234, 2013
M. Pontani and A. Miele, “Periodic Image Trajectories in Earth-Moon Space”, Journal of Optimization Theory and Applications, Vol. 157, No. 3, pp. 866–1887, 2013
M. Pontani and B. A. Conway, “Optimal Low-Thrust Orbital Maneuvers via Indirect Swarming Method”, Journal of Optimization Theory and Applications, Vol. 162, No. 1, pp. 272–292, 2014
M. Pontani and B. A. Conway, “Minimum-Fuel Finite-Thrust Relative Orbit Maneuvers via Indirect Heuristic Method”, Journal of Guidance, Control, and Dynamics, Vol. 38, No. 5, pp. 913–924, 2015
M. Pontani and A. Miele, “Theorem of Optimal Image Trajectories in the Restricted Problem of Three Bodies”, Journal of Optimization Theory and Applications, Vol. 168, No. 3, pp. 992–1013, 2016
L. S. Pontryagin, V. G. Boltyanskii, R. V. Gamkrelidze and E. F. Mishchenko, The Mathematical Theory of Optimal Processes, Princeton University Press, Princeton, NJ, 1962
V. Szebehely, Theory of Orbits - the Restricted Problem of Three Bodies, Academic Press, New York, NY, pp. 7–25, 1967
N. X. Vinh, “General theory of optimal trajectory for rocket flight in a resisting medium”, Journal of Optimization Theory and Applications, Vol. 11, pp. 189–202, 1973
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Pontani, M. Optimal Mirror Trajectories Using Continuous Thrust. Aerotec. Missili Spaz. 96, 204–215 (2017). https://doi.org/10.1007/BF03404755
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DOI: https://doi.org/10.1007/BF03404755