Paper information

Paper code

IAC-19,C1,9,11,x51625

Date

2019-10-25

Time

16:00

Order

11

Room

150A

Title

Optimal Guidance Trajectories for a Nanosatellite Docking with a Tumbling Resident Space Object using a high fidelity J2 and Quadratic Drag Perturbations Model

abstract

View PDF

Session

9. Guidance, Navigation & Control (3)

symposium

C1. IAF ASTRODYNAMICS SYMPOSIUM

congress

IAC-19

Type of presentation

oral

Main author

Mr. Parv Patel, University of Southern California, United States

Co-authors

Dr. Bogdan Udrea, Embry-Riddle Aeronautical University, United States;