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University of Colorado Boulder ASEN 5070: Statistical Orbit Determination I Fall 2014 Professor Brandon A. Jones Lecture 3: Basics of Orbit Propagation
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University of Colorado Boulder Monday is Labor Day! Homework 0 & 1 Due September 5 I am out of town Sept. 9-12 ◦ Would anyone be interested in attending the recording of a lecture? 2
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University of Colorado Boulder Orbital elements – Notes on Implementation Perturbing Forces – Wrap-up Coordinate and Time Systems Flat Earth Problem 3
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University of Colorado Boulder 4 Orbit Elements – Review and Implementation
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University of Colorado Boulder The six orbit elements (or Kepler elements) are constant in the problem of two bodies (two gravitationally attracting spheres, or point masses) ◦ Define shape of the orbit a: semimajor axis e: eccentricity ◦ Define the orientation of the orbit in space i: inclination Ω: angle defining location of ascending node (AN) : angle from AN to perifocus; argument of perifocus ◦ Reference time/angle: t p : time of perifocus (or mean anomaly at specified time) v,M: True or mean anomaly 5
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University of Colorado Boulder a – Size e – Shape v – Position 6
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University of Colorado Boulder i - Inclination Ω - RAAN ω – Arg. of Perigee 7
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University of Colorado Boulder Will get an imaginary number from cos -1 (a) if a=1+1e-16 (for example) The 1e-16 is a result of finite point arithmetic You may need to use something akin to the pseudocode: 8
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University of Colorado Boulder Inverse tangent has an angle ambiguity Better to use atan2() when possible: 9
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University of Colorado Boulder 10 Perturbing Forces – Wrap-up
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University of Colorado Boulder “Potential Energy is energy associated with the relative positions of two or more interacting particles.” It is a function of the relative position ◦ Should it be positive or negative? 11
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University of Colorado Boulder For a conservative system: 12
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University of Colorado Boulder 13 Coordinate and Time Frames
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University of Colorado Boulder 14 Define xyz reference frame (Earth centered, Earth fixed; ECEF or ECF), fixed in the solid (and rigid) Earth and rotates with it Longitude λ measured from Greenwich Meridian 0≤ λ < 360° E; or measure λ East (+) or West (-) Latitude (geocentric latitude) measured from equator (φ is North (+) or South (-)) ◦ At the poles, φ = + 90° N or φ = -90° S
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University of Colorado Boulder 15 The transformation between ECI and ECF is required in the equations of motion ◦ Depends on the current time! ◦ Thanks to Einstein, we know that time is not simple…
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University of Colorado Boulder Countless systems exist to measure the passage of time. To varying degrees, each of the following types is important to the mission analyst: ◦ Atomic Time Unit of duration is defined based on an atomic clock. ◦ Universal Time Unit of duration is designed to represent a mean solar day as uniformly as possible. ◦ Sidereal Time Unit of duration is defined based on Earth’s rotation relative to distant stars. ◦ Dynamical Time Unit of duration is defined based on the orbital motion of the Solar System. 16
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University of Colorado Boulder Question: How do you quantify the passage of time? Year Month Day Second Pendulums Atoms 18 What are some issues with each of these? Gravity Earthquakes Errant elbows
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University of Colorado Boulder Definitions of a Year ◦ Julian Year: 365.25 days, where an SI “day” = 86400 SI “seconds”. ◦ Sidereal Year: 365.256 363 004 mean solar days Duration of time required for Earth to traverse one revolution about the sun, measured via distant star. ◦ Tropical Year: 365.242 19 days Duration of time for Sun’s ecliptic longitude to advance 360 deg. Shorter on account of Earth’s axial precession. ◦ Anomalistic Year: 365.259 636 days Perihelion to perihelion. ◦ Draconic Year: 365.620 075 883 days One ascending lunar node to the next (two lunar eclipse seasons) ◦ Full Moon Cycle, Lunar Year, Vague Year, Heliacal Year, Sothic Year, Gaussian Year, Besselian Year 19
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University of Colorado Boulder Equinox location is function of time ◦ Sun and Moon interact with Earth J2 to produce Precession of equinox (ψ) Nutation (ε) Newtonian time (independent variable of equations of motion) is represented by atomic time scales (dependent on Cesium Clock)
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University of Colorado Boulder Inertial: fixed orientation in space ◦ Inertial coordinate frames are typically tied to hundreds of observations of quasars and other very distant near-fixed objects in the sky. Rotating ◦ Constant angular velocity: mean spin motion of a planet ◦ Osculating angular velocity: accurate spin motion of a planet 21
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University of Colorado Boulder Coordinate Systems = Frame + Origin ◦ Inertial coordinate systems require that the system be non-accelerating. Inertial frame + non-accelerating origin ◦ “Inertial” coordinate systems are usually just non- rotating coordinate systems. 22
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University of Colorado Boulder Converting from ECI to ECF 23 P is the precession matrix (~50 arcsec/yr) N is the nutation matrix (main term is 9 arcsec with 18.6 yr period) S’ is sidereal rotation (depends on changes in angular velocity magnitude; UT1) W is polar motion ◦ Earth Orientation Parameters Caution: small effects may be important in particular application
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University of Colorado Boulder We did not spend a lot of time on this subject, but it is very, very important to orbit determination! What impact can the coordinates and time have on propagation and observing a spacecraft? 24
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University of Colorado Boulder 25 Flat Earth Problem
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University of Colorado Boulder Assume linear motion: 27
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University of Colorado Boulder Given an error-free state at a time t, we can solve for the state at t 0 What about when we have a different observation type? 28
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University of Colorado Boulder Relationship between the estimated state and the observations is no longer linear For our purposes, let’s assume the station coordinates are known. You will solve one case of this problem for HW 1, Prob. 6 29
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