Trajectory Analysis Between Quasi-Periodic Orbits and the Lagrangian Points Around Phobos

Pedro J. Llanos; Jesus D, Jordan; Gerald R. Hintz; Manuel Sanjurjo-Rivo; Pedro J Llanos de la Concha

doi:10.2514/6.2014-4349

Trajectory Analysis Between Quasi-Periodic Orbits and the Lagrangian Points Around Phobos

Pedro J. Llanos, Jesus D, Jordan, Gerald R. Hintz, Manuel Sanjurjo-Rivo, Pedro J Llanos de la Concha

Research output: Contribution to conference › Presentation

Abstract

This paper proposes novel orbits in the Circular Restricted Three-Body Problem (CRTBP) of the Mars-Phobos system. We have found different types of quasiperiodic orbits with long-term stability that can be connected into the invariant manifolds that transport the spacecraft directly into a L1 halo orbit. We analyze the feasibility of several transfer trajectories connecting different sizes of halo orbits around L1 and L2. We further analyze the station-keeping maneuvers for the halo orbits around the collinear libration points allowing the spacecraft to stay for several

days and increase the science performed during proximity operations in the vicinity of Phobos.

Original language	American English
DOIs	https://doi.org/10.2514/6.2014-4349
State	Published - Aug 2014
Event	AIAA/AAS Astrodynamics Specialist Conference - San Diego, CA Duration: Aug 1 2014 → …

Conference

Conference	AIAA/AAS Astrodynamics Specialist Conference
Period	8/1/14 → …

Keywords

Circular-Restricted Three-Body Problem
Phobos
Mars
quasi-periodic orbits

Disciplines

Navigation, Guidance, Control and Dynamics
Space Vehicles

Access to Document

10.2514/6.2014-4349License: Unspecified

Cite this

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title = "Trajectory Analysis Between Quasi-Periodic Orbits and the Lagrangian Points Around Phobos",

abstract = " This paper proposes novel orbits in the Circular Restricted Three-Body Problem (CRTBP) of the Mars-Phobos system. We have found different types of quasiperiodic orbits with long-term stability that can be connected into the invariant manifolds that transport the spacecraft directly into a L1 halo orbit. We analyze the feasibility of several transfer trajectories connecting different sizes of halo orbits around L1 and L2. We further analyze the station-keeping maneuvers for the halo orbits around the collinear libration points allowing the spacecraft to stay for several days and increase the science performed during proximity operations in the vicinity of Phobos.",

keywords = "Circular-Restricted Three-Body Problem, Phobos, Mars, quasi-periodic orbits",

author = "Llanos, {Pedro J.} and Jordan, {Jesus D,} and Hintz, {Gerald R.} and Manuel Sanjurjo-Rivo and {Llanos de la Concha}, {Pedro J}",

year = "2014",

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doi = "10.2514/6.2014-4349",

language = "American English",

note = "AIAA/AAS Astrodynamics Specialist Conference ; Conference date: 01-08-2014",

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T1 - Trajectory Analysis Between Quasi-Periodic Orbits and the Lagrangian Points Around Phobos

AU - Llanos, Pedro J.

AU - Jordan, Jesus D,

AU - Hintz, Gerald R.

AU - Sanjurjo-Rivo, Manuel

AU - Llanos de la Concha, Pedro J

PY - 2014/8

Y1 - 2014/8

N2 - This paper proposes novel orbits in the Circular Restricted Three-Body Problem (CRTBP) of the Mars-Phobos system. We have found different types of quasiperiodic orbits with long-term stability that can be connected into the invariant manifolds that transport the spacecraft directly into a L1 halo orbit. We analyze the feasibility of several transfer trajectories connecting different sizes of halo orbits around L1 and L2. We further analyze the station-keeping maneuvers for the halo orbits around the collinear libration points allowing the spacecraft to stay for several days and increase the science performed during proximity operations in the vicinity of Phobos.

AB - This paper proposes novel orbits in the Circular Restricted Three-Body Problem (CRTBP) of the Mars-Phobos system. We have found different types of quasiperiodic orbits with long-term stability that can be connected into the invariant manifolds that transport the spacecraft directly into a L1 halo orbit. We analyze the feasibility of several transfer trajectories connecting different sizes of halo orbits around L1 and L2. We further analyze the station-keeping maneuvers for the halo orbits around the collinear libration points allowing the spacecraft to stay for several days and increase the science performed during proximity operations in the vicinity of Phobos.

KW - Circular-Restricted Three-Body Problem

KW - Phobos

KW - Mars

KW - quasi-periodic orbits

U2 - 10.2514/6.2014-4349

DO - 10.2514/6.2014-4349

M3 - Presentation

T2 - AIAA/AAS Astrodynamics Specialist Conference

Y2 - 1 August 2014

ER -