Hybrid algorithm for multiple gravity-assist and impulsive delta-V maneuvers

S Wagner, B Wie - Journal of Guidance, Control, and Dynamics, 2015 - arc.aiaa.org
A combination of multiple gravity-assist and impulsive Delta-V maneuvers is often required
for interplanetary and interstellar space missions, such as NASA's Voyager 1 and 2, Galileo …

Multi-fidelity approach for global trajectory optimization using GPU-based highly parallel architecture

S Ueda, H Ogawa - Aerospace Science and Technology, 2021 - Elsevier
A flexible and robust design space search method based on a systematic approach as well
as effective optimization algorithms is required to accomplish challenging space missions …

[PDF][PDF] An adaptive multi-spline refinement algorithm in simulation based sailboat trajectory optimization using onboard multi-core computer systems

R Dębski - International Journal of Applied Mathematics and …, 2016 - sciendo.com
A new dynamic programming based parallel algorithm adapted to on-board heterogeneous
computers for simulation based trajectory optimization is studied in the context of “high …

Responsive theater maneuvers via particle swarm optimization

DJ Showalter, JT Black - Journal of Spacecraft and Rockets, 2014 - arc.aiaa.org
This research investigates the performance of the particle swarm optimization algorithm in
the solution of responsive theater maneuvers, introduced here for the first time. The …

Target selection for a hypervelocity asteroid intercept vehicle flight validation mission

S Wagner, B Wie, BW Barbee - Acta Astronautica, 2015 - Elsevier
Asteroids and comets have collided with the Earth in the past and will do so again in the
future. Throughout Earth׳ s history these collisions have played a significant role in shaping …

Automated trajectory design for impulsive and low thrust interplanetary mission analysis

SA Wagner - 2014 - search.proquest.com
This dissertation describes a hybrid optimization algorithm that is able to determine optimal
trajectories for many complex mission analysis and design orbital mechanics problems. This …

Simulation-based sailboat trajectory optimization using on-board heterogeneous computers

R Dębski - Computer Science, 2016 - yadda.icm.edu.pl
A dynamic programming-based algorithm adapted to on-board heterogeneous computers
for simulation-based trajectory optimization was studied in the context of high-performance …

[PDF][PDF] Development of an asteroid mission design software tool for planetary defense

G Vardaxis, B Wie - 3rd Planetary Defense Conference. Flagstaff …, 2013 - iaaspace.org
When the impact threat of an identified potentially hazardous near-Earth objects (NEO)
becomes serious, the development and design of asteroid deflection/disruption missions …

Optimal Continuous-Thrust Responsive Theater Maneuvers

DJ Showalter, JT Black - Journal of Spacecraft and Rockets, 2015 - arc.aiaa.org
This research investigates a continuous-thrust implementation of the responsive theater
maneuver, which is designed to alter a spacecraft's entry conditions as it overflies a …

[PDF][PDF] Feasibility Study of Orbit Control Methods in CubeSats with Electric Propulsion for an Interplanetary Mission Pallavi Prasad, Yassir Debbah, Gabriel Valles …

V Priyanka, A Balaji, D Wischert - 2022 - researchgate.net
Abstract With ESA Science Programme Voyage 2050, there is a need for technology
developments in terms of more efficient power and propulsion systems for future space …