15
79%
master: 69%

Ran 22 Jan 2017 01:31AM UTC

Jobs 1

Files 11

Run time 1s

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Build # 15

Build Type

push

travis-ci

Committed by

ChristopherRabotin

Commit Message

Fixes #39 by doing an approximation

*Note:* for a true circular or equatorial orbit, one now needs to
initialize the orbit with NewOrbitFromOE and then overwrite the
eccentricity and the inclination manually. Otherwise, one can also just
provide the R and V vectors in NewOrbitFromRV.

Issue with Hohmann: PROP does not support normalization, so I need to
see how to handle that without breaking the continuous thrust.

Run Details

1059 of 1369 relevant lines covered (77.36%)

11335624.49 hits per line

Jobs

ID	Job ID	Ran	Files	Coverage
1	15.1 (-VSOP87=./data/vsop87 -DATAOUT=./outputdata)	22 Jan 2017 01:31AM UTC	0	77.36	Travis Job 15.1

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