Controlling chaos and analysis of the dynamics of collective motion of satellite in formation flight

• Grant number: 08/06066-5
• Support Opportunities: Scholarships in Brazil - Doctorate
• Start date: May 01, 2009
• End date: October 31, 2012
• Field of knowledge: Engineering - Electrical Engineering - Industrial Electronics, Electronic Systems and Controls
• Principal Investigator: Elbert Einstein Nehrer Macau
• Grantee: Francisco Javier Tipán Salazar
• Host Institution: Instituto Nacional de Pesquisas Espaciais (INPE). Ministério da Ciência, Tecnologia e Inovação (Brasil). São José dos Campos , SP, Brazil
• Associated research grant: 06/04997-6 - Close approach problems in orbital dynamics, AP.TEM

Scientific publications

(9)

(References retrieved automatically from Web of Science and SciELO through information on FAPESP grants and their corresponding numbers as mentioned in the publications by the authors)

SALAZAR, F. J. T.; MACAU, E. E. N.; WINTER, O. C.. Pareto Frontier for the time-energy cost vector to an Earth-Moon transfer orbit using the patched-conic approximation. COMPUTATIONAL & APPLIED MATHEMATICS, v. 34, n. 2, p. 461-475, JUL 2015. (11/08171-3, 08/06066-5, 13/03233-6)

SALAZAR, F. J. T.; DE MELO, C. F.; MACAU, E. E. N.; WINTER, O. C.. Three-body problem, its Lagrangian points and how to exploit them using an alternative transfer to L4 and L5. CELESTIAL MECHANICS & DYNAMICAL ASTRONOMY, v. 114, n. 1-2, SI, p. 201-213, OCT 2012. (08/06066-5)

SALAZAR, F. J. T.; WINTER, O. C.; MACAU, E. E.; MASDEMONT, J. J.; GOMEZ, G.. Zero drift regions and control strategies to keep satellite in formation around triangular libration point in the restricted Sun-Earth-Moon scenario. Advances in Space Research, v. 56, n. 7, p. 1502-1518, OCT 1 2015. (08/06066-5, 11/08171-3, 15/00559-3, 11/50151-0, 13/03233-6)

SALAZAR, F. J. T.; MACAU, E. E. N.; WINTER, O. C.. Pareto Frontier for the time-energy cost vector to an Earth-Moon transfer orbit using the patched-conic approximation. COMPUTATIONAL & APPLIED MATHEMATICS, v. 34, n. 2, p. 15-pg., 2015-07-01. (08/06066-5, 13/03233-6, 11/08171-3)

SALAZAR, F. J. T.; MASDEMONT, J. J.; GOMEZ, G.; MACAU, E. E.; WINTER, O. C.. Zero, minimum and maximum relative radial acceleration for planar formation flight dynamics near triangular libration points in the Earth-Moon system. Advances in Space Research, v. 54, n. 9, p. 1838-1857, NOV 1 2014. (11/08171-3, 08/06066-5, 11/50151-0, 13/03233-6)

SALAZAR, F. J. T.; MACAU, E. E. N.; WINTER, O. C.. Alternative transfer to the Earth-Moon Lagrangian points L4 and L5 using lunar gravity assist. Advances in Space Research, v. 53, n. 3, p. 543-557, FEB 1 2014. (11/08171-3, 08/06066-5, 13/03233-6)

SALAZAR, F. J. T.; MACAU, E. E. N.; WINTER, O. C.. Chaotic Dynamics in a Low-Energy Transfer Strategy to the Equilateral Equilibrium Points in the Earth-Moon System. INTERNATIONAL JOURNAL OF BIFURCATION AND CHAOS, v. 25, n. 5, MAY 2015. (11/08171-3, 08/06066-5, 11/50151-0, 13/03233-6)

SALAZAR, F. J. T.; WINTER, O. C.; MACAU, E. E.; MASDEMONT, J. J.; GOMEZ, G.. Natural formations at the Earth-Moon triangular point in perturbed restricted problems. Advances in Space Research, v. 56, n. 1, p. 144-162, JUL 1 2015. (11/08171-3, 08/06066-5, 11/50151-0, 13/03233-6)

SALAZAR, F. J. T.; DE MELO, C. F.; MACAU, E. E. N.; WINTER, O. C.. Three-body problem, its Lagrangian points and how to exploit them using an alternative transfer to L4 and L5. CELESTIAL MECHANICS & DYNAMICAL ASTRONOMY, v. 114, n. 1-2, p. 13-pg., 2012-10-01. (08/06066-5)