Four-Impulsive Rendezvous Maneuvers for Spacecrafts in Circular Orbits Using Genetic Algorithms

Autor(es)

Souza dos Santos, Denilson Paulo ^[1] ; Bertachini de Almeida Prado, Antonio Fernando ^[1] ; Colasurdo, Guido ^[2]

Afiliação do(s) autor(es)

^[1] Div Space Mech & Control INPE, BR-12227310 Sao Jose Dos Campos, SP - Brazil

^[2] Univ Roma La Sapienza, Dept Aerosp & Mech Engn, I-00185 Rome - Italy

• Tipo de documento: Artigo Científico
• Fonte: MATHEMATICAL PROBLEMS IN ENGINEERING; 2012.
• Citações Web of Science: 4

Resumo

Spacecraft maneuvers is a very important topic in aerospace engineering activities today. In a more generic way, a spacecraft maneuver has the objective of transferring a spacecraft from one orbit to another, taking into account some restrictions. In the present paper, the problem of rendezvous is considered. In this type of problem, it is necessary to transfer a spacecraft from one orbit to another, but with the extra constraint of meeting another spacecraft when reaching the final orbit. In particular, the present paper aims to analyze rendezvous maneuvers between two coplanar circular orbits, seeking to perform this transfer with lowest possible fuel consumption, assuming that this problem is time-free and using four burns during the process. The assumption of four burns is used to represent a constraint posed by a real mission. Then, a genetic algorithm is used to solve the problem. After that, a study is made for a maneuver that will make a spacecraft to encounter a planet, in order to make a close approach that will change its energy. Several simulations are presented. (AU)

• Processo FAPESP: 09/16517-7 - Otimização de trajetórias espaciais utilizando propulsão elétrica solar e manobras gravitacionalmente assistidas, com algoritmo genético
• Beneficiário: Denilson Paulo Souza dos Santos
• Linha de fomento: Bolsas no Brasil - Pós-Doutorado