Orbital mission analysis for a lunar mapping satellite

Sang-Young Park, John L. Junkins

Research output: Contribution to conferencePaper

2 Citations (Scopus)

Abstract

Using a frozen orbit concept, we establish a new lunar mapping orbit which is near circular, near polar, near constant low altitude, and near sun-synchronous. A proper orbit is one whose mean elements are constant, except for uniform precession of the line of nodes and periapsis over a month, and periodic element variations are suitably small. With the INT lunar gravity model, we find a family frozen orbits that are near polar, so global coverage can be achieved in one month. This family of frozen orbits yields an attractive set of lunar mapping orbits with 100 km altitude and good control over sunlight conditions.

Original languageEnglish
Pages93-98
Number of pages6
Publication statusPublished - 1994 Jan 1
EventAstrodynamics Conference, 1994 - Scottsdale, United States
Duration: 1994 Aug 11994 Aug 3

Other

OtherAstrodynamics Conference, 1994
CountryUnited States
CityScottsdale
Period94/8/194/8/3

Fingerprint

orbits
orbitals
altitude control
low altitude
sunlight
precession
sun
gravitation

All Science Journal Classification (ASJC) codes

  • Astronomy and Astrophysics

Cite this

Park, S-Y., & Junkins, J. L. (1994). Orbital mission analysis for a lunar mapping satellite. 93-98. Paper presented at Astrodynamics Conference, 1994, Scottsdale, United States.
Park, Sang-Young ; Junkins, John L. / Orbital mission analysis for a lunar mapping satellite. Paper presented at Astrodynamics Conference, 1994, Scottsdale, United States.6 p.
@conference{2046d8873a3641cc9e5921d51b833573,
title = "Orbital mission analysis for a lunar mapping satellite",
abstract = "Using a frozen orbit concept, we establish a new lunar mapping orbit which is near circular, near polar, near constant low altitude, and near sun-synchronous. A proper orbit is one whose mean elements are constant, except for uniform precession of the line of nodes and periapsis over a month, and periodic element variations are suitably small. With the INT lunar gravity model, we find a family frozen orbits that are near polar, so global coverage can be achieved in one month. This family of frozen orbits yields an attractive set of lunar mapping orbits with 100 km altitude and good control over sunlight conditions.",
author = "Sang-Young Park and Junkins, {John L.}",
year = "1994",
month = "1",
day = "1",
language = "English",
pages = "93--98",
note = "Astrodynamics Conference, 1994 ; Conference date: 01-08-1994 Through 03-08-1994",

}

Park, S-Y & Junkins, JL 1994, 'Orbital mission analysis for a lunar mapping satellite' Paper presented at Astrodynamics Conference, 1994, Scottsdale, United States, 94/8/1 - 94/8/3, pp. 93-98.

Orbital mission analysis for a lunar mapping satellite. / Park, Sang-Young; Junkins, John L.

1994. 93-98 Paper presented at Astrodynamics Conference, 1994, Scottsdale, United States.

Research output: Contribution to conferencePaper

TY - CONF

T1 - Orbital mission analysis for a lunar mapping satellite

AU - Park, Sang-Young

AU - Junkins, John L.

PY - 1994/1/1

Y1 - 1994/1/1

N2 - Using a frozen orbit concept, we establish a new lunar mapping orbit which is near circular, near polar, near constant low altitude, and near sun-synchronous. A proper orbit is one whose mean elements are constant, except for uniform precession of the line of nodes and periapsis over a month, and periodic element variations are suitably small. With the INT lunar gravity model, we find a family frozen orbits that are near polar, so global coverage can be achieved in one month. This family of frozen orbits yields an attractive set of lunar mapping orbits with 100 km altitude and good control over sunlight conditions.

AB - Using a frozen orbit concept, we establish a new lunar mapping orbit which is near circular, near polar, near constant low altitude, and near sun-synchronous. A proper orbit is one whose mean elements are constant, except for uniform precession of the line of nodes and periapsis over a month, and periodic element variations are suitably small. With the INT lunar gravity model, we find a family frozen orbits that are near polar, so global coverage can be achieved in one month. This family of frozen orbits yields an attractive set of lunar mapping orbits with 100 km altitude and good control over sunlight conditions.

UR - http://www.scopus.com/inward/record.url?scp=84999015261&partnerID=8YFLogxK

UR - http://www.scopus.com/inward/citedby.url?scp=84999015261&partnerID=8YFLogxK

M3 - Paper

SP - 93

EP - 98

ER -

Park S-Y, Junkins JL. Orbital mission analysis for a lunar mapping satellite. 1994. Paper presented at Astrodynamics Conference, 1994, Scottsdale, United States.