University of Colorado Boulder ASEN 5070 Statistical Orbit determination I Fall 2012 Professor George H. Born Professor Jeffrey S. Parker Lecture 6: Launches.

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Presentation transcript:

University of Colorado Boulder ASEN 5070 Statistical Orbit determination I Fall 2012 Professor George H. Born Professor Jeffrey S. Parker Lecture 6: Launches and Spaceflight Ops 1

University of Colorado Boulder  Homework 2 due Today  Homework 3 due next week  Atlas 5 Launch! 2

University of Colorado Boulder  Plan: watch Atlas V launch  Discuss where Stat OD comes in  Talk about Spaceflight Ops  Return to Quiz results, statistics, etc 3

University of Colorado Boulder  Spaceflight Now  3:39pm launch time 4

University of Colorado Boulder  Ground stations (including ships) track launches.  In the past, people would use visual observations (compasses, protractors, etc)  Now, mostly radar 5

University of Colorado Boulder  Every launch system works differently  Solid vs. Liquid systems  Active vs. Passive guidance systems  Feedback vs. Seat-of-the-Pants systems  Measurements: IMUs, accelerometers, gyros, GPS, etc. 6

University of Colorado Boulder  Delta and Atlas launch vehicles are historically very accurate ◦ Liquid core and upper stages ◦ Well-characterized systems ◦ Good feedback with measurements ◦ Expensive  Pegasus, Minotaur IV less accurate, but not bad ◦ Pegasus accuracy:  Injection apse: +/- 10 km (3-sigma)  Opposite apse: +/- 80 km ◦ Minotaur accuracy:  Injection apse: +/- 5 km (3-sigma)  Opposite apse: +/- 25 km ◦ Minotaur IV is essentially three Peacekeeper ICBMs stacked on top of each other. ◦ Orion 38 4 th stage may be used to improve injection accuracy. Optional Star 48 not-so-much. ◦ 7

University of Colorado Boulder  Launch services provide an estimate of the spacecraft’s trajectory and a corresponding covariance matrix. 8

University of Colorado Boulder  The Stat OD process then takes the estimate of the spacecraft trajectory:  And the covariance  And uses those to initialize the Stat OD process. 9

University of Colorado Boulder  The Stat OD process then takes the estimate of the spacecraft trajectory:  And the covariance  And uses those to initialize the Stat OD process.  Observations update these 10 New covariance New estimate

University of Colorado Boulder  Brief Switch to Mars Odyssey Example 11

University of Colorado Boulder  Some popular questions and answers  Grading, code, etc  Comments may be audio files 12

University of Colorado Boulder  Some popular questions and answers  Energy tolerance, compared to solutions 13

University of Colorado Boulder  Questions yet? 14