Search Results - "Lantoine, Gregory"
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A Hybrid Differential Dynamic Programming Algorithm for Constrained Optimal Control Problems. Part 1: Theory
Published in Journal of optimization theory and applications (01-08-2012)“…A new algorithm is presented to solve constrained nonlinear optimal control problems, with an emphasis on highly nonlinear dynamical systems. The algorithm,…”
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Journal Article -
2
A Hybrid Differential Dynamic Programming Algorithm for Constrained Optimal Control Problems. Part 2: Application
Published in Journal of optimization theory and applications (01-08-2012)“…In the first part of this paper series, a new solver, called HDDP, was presented for solving constrained, nonlinear optimal control problems. In the present…”
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3
Broad search for unstable resonant orbits in the planar circular restricted three-body problem
Published in Celestial mechanics and dynamical astronomy (01-02-2016)“…Unstable resonant orbits in the circular restricted three-body problem have increasingly been used for trajectory design using optimization and invariant…”
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4
Quasi-terminator orbits near primitive bodies
Published in Celestial mechanics and dynamical astronomy (01-10-2014)“…Quasi-terminator orbits are introduced as a class of quasi-periodic trajectories in the solar radiation pressure (SRP) perturbed Hill dynamics. These orbits…”
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Optimization of low-energy resonant hopping transfers between planetary moons
Published in Acta astronautica (01-04-2011)“…In response to the scientific interest in Jupiter's Galilean moons, NASA and ESA have plans to send orbiting missions to Europa and Ganymede, respectively. The…”
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Indirect trajectory optimization via solar sailing primer vector theory: Minimum solar-angle transfers
Published in Acta astronautica (01-10-2023)“…Building upon the recent development of solar sailing primer vector theory and its successful applications, we propose a new formulation for indirect…”
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7
Design Of Lunar-Gravity-Assisted Escape Trajectories
Published in The Journal of the astronautical sciences (01-12-2020)“…Lunar gravity assist is a means to boost the energy and C3 of an escape trajectory. Trajectories with two lunar gravity assists are considered and analyzed…”
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Science orbit design with a quasi-frozen beta angle: effects of body obliquity on J2-perturbed dynamics
Published in Celestial mechanics and dynamical astronomy (01-10-2020)“…The beta angle, an angle formed by the sunlight and a spacecraft orbital plane, is an important parameter for science orbit design of orbiter missions. This…”
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Trajectory & maneuver design of the NEA Scout solar sail mission
Published in Acta astronautica (01-12-2024)“…The Near-Earth Asteroid Scout (NEA Scout) mission aimed to deliver a 6U CubeSat to a slow flyby of a Near Earth Asteroid using a solar sail as the primary…”
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Near Ballistic Halo-to-Halo Transfers between Planetary Moons
Published in The Journal of the astronautical sciences (01-07-2011)“…Intermoon transfers are important components of planetary tour missions. However, these transfers are challenging to design due in part to the chaotic…”
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Complete closed-form solutions of the Stark problem
Published in Celestial mechanics and dynamical astronomy (01-04-2011)“…Perturbed two-body problems play a special role in Celestial Mechanics as they capture the dominant dynamics for a broad range of natural and artificial…”
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A study on simultaneous design of a Hall Effect Thruster and its low-thrust trajectory
Published in Acta astronautica (01-02-2016)“…Space missions involving Hall Effect Thrusters are more and more common, and designs of both Hall Effect Thrusters and low-thrust trajectories require more…”
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13
Magnetour: Surfing planetary systems on electromagnetic and multi-body gravity fields
Published in Acta astronautica (01-09-2017)“…A comprehensive tour of the complex outer planet systems is a central goal in space science. However, orbiting multiple moons of the same planet would be…”
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Journal Article -
14
Near Ballistic Halo-to-Halo Transfers between Planetary Moons
Published in The Journal of the astronautical sciences (01-09-2011)“…Intermoon transfers are important components of planetary tour missions. However, these transfers are challenging to design due in part to the chaotic…”
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Journal Article -
15
Optimal Control of Relative Motion in Arbitrary Fields: Application at Deimos
Published in The Journal of the astronautical sciences (01-06-2012)“…A second-order, general dynamics, relative motion framework is formulated to solve for optimal finite-burn transfers in complex gravity fields that are not…”
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Remote sensing of venusian seismic activity with a small spacecraft, the VAMOS mission concept
Published in 2018 IEEE Aerospace Conference (01-03-2018)“…The Venusian atmosphere creates inhospitable temperature and pressure conditions for the surface of Venus, Earth's twin planet, making in-situ measurements of…”
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Conference Proceeding -
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Psyche: Journey to a metal world
Published in 2017 IEEE Aerospace Conference (01-03-2017)“…In September 2015, NASA selected five mission concepts from a field of 27 to proceed to the next stage (step 2) of the latest Discovery mission competition…”
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Conference Proceeding -
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NASA's Lunar Trailblazer Mission: A Pioneering Small Satellite for Lunar Water and Lunar Geology
Published in 2022 IEEE Aerospace Conference (AERO) (05-03-2022)“…Selected in 2019 as a NASA SIMPLEx mission, Lunar Trailblazer is in implementation for flight system delivery at the end of 2022. The mission's goal is to…”
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Conference Proceeding -
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Human-assisted Mars Sample Return
Published in 2015 IEEE Aerospace Conference (01-03-2015)“…Any Mars Sample Return campaign must assure a very low probability of inadvertent release of Mars material into the Earth's biosphere in order to provide…”
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Conference Proceeding -
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A methodology for robust optimization of low-thrust trajectories in multi-body environments
Published 01-01-2010“…Future ambitious solar system exploration missions are likely to require ever larger propulsion capabilities and involve innovative interplanetary trajectories…”
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Dissertation