SCOPUS 정보 검색 플랫폼

Volumn 128, Issue 3 1785, 2004, Pages 1455-1464

Efficient orbit integration by the orbital longitude method using antifocal anomaly

Author keywords

Celestial mechanics; Methods: n body simulations

Indexed keywords

EID: 7944228695 PISSN: 00046256 EISSN: None Source Type: Journal
DOI: 10.1086/423042 Document Type: Article

Times cited : (11)

References (7)

1
- 0141640856
- Paper I
- Fukushima, T. 2003a, AJ, 126, 1097 (Paper I)
- (2003) AJ , vol.126 , pp. 1097
- Fukushima, T.¹

2
- 0348199187
- Paper II
- -. 2003b, AJ, 126, 2567 (Paper II)
- (2003) AJ , vol.126 , pp. 2567

3
- 1642299022
- Paper III
- -. 2003c, AJ, 126, 3138 (Paper III)
- (2003) AJ , vol.126 , pp. 3138

4
- 3142762423
- Paper IV
- -. 2004a, AJ, 127, 3638 (Paper IV)
- (2004) AJ , vol.127 , pp. 3638

5
- 4544379446
- Paper V
- Fukushima, T. 2004b, AJ, 128, 920 (Paper V).
- (2004) AJ , vol.128 , pp. 920
- Fukushima, T.¹

6
- 7944230652
- Paper VI
- -. 2004c, AJ, 128, 1446 (Paper VI)
- (2004) AJ , vol.128 , pp. 1446

7
- 7944225993
- submitted (Paper VII)
- -. 2004d, Celest. Mech. Dyn. Astron., submitted (Paper VII)
- (2004) Celest. Mech. Dyn. Astron.

* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.