session 7

1

13:45

Optimal Low-Thrust Earth-Moon Orbit Transfers via Multiple-arc Formulation and Implicit Costate Transformation

15

confirmed

Dr. Mauro Pontani

Sapienza University of Rome

Italy

2

14:00

optimal trajectory design by adam under stochastic disturbing acceleration

15

confirmed

Mr. Shodai Hirayama

Kyushu University

Japan

3

14:15

Multi-objective optimization of lunar communication/navigation constellations based on LPOs and DROs

15

confirmed

Mr. Yuchen He

Beihang University

China

4

14:30

Matryoshka Orbital Networks

15

confirmed

Mr. Joshua Gribben

University of Strathclyde

United Kingdom

5

14:45

Many-to-many GEO on-orbit refueling mission optimization under time-varying fuel demands via modified differential evolution

15

confirmed

Prof. Chuanjiang Li

Harbin Institute of Technology

China

6

15:00

Optimizing Launch Window Opportunities for ESA’s Comet Interceptor Mission using Prime Vector Theory

15

confirmed

Mr. Miguel Rebelo

ISAE-Supaero University of Toulouse

France

7

15:15

Extended Perilune Rendezvous Method for Low Delta-V Transition to NRHO

15

confirmed

Mr. Junji Kikuchi

Japan Aerospace Exploration Agency (JAXA)

Japan

8

15:30

Extremely Low earth orbit Imaging and Technology Explorer (ELITE): Pushing earth observation boundaries

15

confirmed

Prof. Erick Lansard

Nanyang Technological University

Singapore, Republic of

9

15:45

Approximate closed-form solution of the periodically perturbed two-body problem with application to low-thrust optimization

15

confirmed

Mr. Kirill Suslov

Keldysh Institute of Applied Mathematics, RAS

Russian Federation

10

16:00

Optimization of Non-Differentiable Travelling Salesman Problem for Space Trajectory Design with Non-branching Operation

15

confirmed

Prof. Arun Misra

McGill Univeristy

Canada

4*

14:30

Game of cat and mouse in space through multi-objective optimization

15

withdrawn

Mr. Thibault Lebeke

Exotrail

France