Title: MA 4362 Astrodynamics
1MA 4362 Astrodynamics
Orbit Perturbations and Orbit Decay
Chapter 8,Sellers sections 8.2, 8.3 (pp. 272-283)
Week 9
2The N-Body Problem
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4What are Other factors that Perturb the Orbit?
- Any disturbance in the regular motion of a
satellite resulting from a force other than those
causing regular motion - Non-spherical earth (Oblateness)
- Sun/moon/planets gravity(Third bodies)
- Atmospheric drag
5The Earth is Not a Perfect Sphere
In actuality, Earth is an Ellipsoid
6Equatorial Bulge
7Gravitational Potential Theory
Irregularities in the Earths Gravitational Field
are modeled by a complex mathematical Model
referred to as Potential Theory (Laplaces
equation)
8Gravitational Potential Theory
J1 --gt Gravitational Potential of Spherical
earth J2 --gt Accounts for Equatorial Bulge
So-named J2 Effect
J2 -- torques the orbit
9Precession of the Right Ascension(J2 Nodal
Regression)
10Precession of the Right Ascension(Nodal
Regression)
11Sun-Synchronous Orbit
- Approx 98 degree Inclination
- Circular or Elliptical LEO
- Sun Angle is Always same (more later)
- Missions
- Electro Optical Imaging
- Weather (DMSP)
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GROUND TRACE
12Sun Synchronous Orbit
Takes Advantage of the fact that precession of
the line of nodes is the same rate as the earths
angular velocity around the sun (about 0.9856?
per day) (retrograde orbits)
Summer
Spring
Fall
Winter
13Sun Synchronous Orbit (concluded)
14Another J2 Effect Perigee Rotation
- Orbit rotates in orbital plane
15Variation of Argument of Perigee
16Variation of Argument of Perigee
Perigee does not rotate
17Molniya Orbits
Molniya Orbits exploit this quirk of nature
- 63.4 /116.6 Degree Inclination
- 500 km perigee - 40,000 km apogee
- Missions Comm / Surveillance
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21Atmospheric Drag
22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 37 38 39 40 41 42 43 44Numerical Example Orbit Decay of Russian Zarya
Module WHAT IF ENGINE QUIT WORKING ?
45 Russian Zarya Module
46 Russian Zarya Module
47 Russian Zarya Module
48 Russian Zarya Module
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