Combined System–Trajectory Design for Geostationary Orbit Platforms on Hybrid Transfer-Reference-Cited by-同舟云学术

Combined System–Trajectory Design for Geostationary Orbit Platforms on Hybrid Transfer

Published:2021-10-13 Issue: Volume: Page:1-19
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Ceccherini Simone¹^ORCID,Mani Karthik V.¹,Topputo Francesco¹^ORCID

Affiliation:

1. Polytechnic University of Milan, 20156 Milan, Italy

Funder

Regione Lombardia

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.A35012

Reference38 articles.

1. Optimal Planetary Orbital Transfers via Chemical Engines and Electrical Engines

2. The Annual Compendium of Commercial Space Transportation: 2018, Bryce Space and Technology for the Federal Aviation Administration, Vol. 1, No. 1, Washington, D.C., Jan. 2018, pp. 45–52.

3. Advanced Propulsion for Geostationary Orbit Insertion and North-South Station Keeping

4. SackettL. L.MalchowH. L.EdelbaumT. N. “Solar Electric Geocentric Transfer with Attitude Constraints: Analysis,” NASA CR-134927, 1975.

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