TY - GEN
T1 - On earth-moon transfer trajectory with gravitational capture
AU - Yamakawa, Hiroshi
AU - Kawaguchi, Jun'ichiro
AU - Ishii, NObuaki
AU - Matsuo, Hiroki
PY - 1993
Y1 - 1993
N2 - Approaching from outside the sphere of influence, a particle may attain low relative velocity was a celestial body and even rotate around it temporarily, without utilizing any other effects than gravitational force. This mechanism is called gravitational capture (i.e. ballistic capture) and it has been considered to be one of the mechanisms which can explain the origin of planetary satellites. In astrodynamics field, lunar gravitational capture is applied to earth-moon transfer trajectory along with positive use of solar perturbation, paying attention to small delta-V required at lunar orbit insertion. In this paper, from the viewpoint of local two-body energy variation, the mechanism of gravitational capture is analytically investigated. Furthermore, a systematic design method for earth-moon transfer trajectory followed by gravitational capture is established.
AB - Approaching from outside the sphere of influence, a particle may attain low relative velocity was a celestial body and even rotate around it temporarily, without utilizing any other effects than gravitational force. This mechanism is called gravitational capture (i.e. ballistic capture) and it has been considered to be one of the mechanisms which can explain the origin of planetary satellites. In astrodynamics field, lunar gravitational capture is applied to earth-moon transfer trajectory along with positive use of solar perturbation, paying attention to small delta-V required at lunar orbit insertion. In this paper, from the viewpoint of local two-body energy variation, the mechanism of gravitational capture is analytically investigated. Furthermore, a systematic design method for earth-moon transfer trajectory followed by gravitational capture is established.
UR - http://www.scopus.com/inward/record.url?scp=0027725477&partnerID=8YFLogxK
M3 - Conference contribution
AN - SCOPUS:0027725477
SN - 0877033803
T3 - Advances in the Astronautical Sciences
SP - 397
EP - 416
BT - Advances in the Astronautical Sciences
PB - Publ by Univelt Inc
T2 - Proceedings of the AAS/AIAA Astrodynamics Conference. Part 3 (of 3)
Y2 - 16 August 1993 through 19 August 1993
ER -