orbital_shipping

Author	SHA1	Message	Date
cinnaboot	88f2de41a4	fix typo in test case description	4 years ago
cinnaboot	8a05d11390	add orbit determination test case for flight path angle	4 years ago
cinnaboot	157e770bb8	add test case for orbit shaping	4 years ago
cinnaboot	c76c7c6ae6	add test case for equatorial orbit	4 years ago
cinnaboot	a3dfae36c4	add function to convert orbital elements to state vectors	4 years ago
cinnaboot	c3a95370cb	add test case for vectors to orbital elements	4 years ago
cinnaboot	f3d792897a	use double precision floats in test	4 years ago
cinnaboot	0a2e01909d	add functions to convert orbital elements to state vectors	4 years ago
cinnaboot	cc934945de	impletment multiple orbits	4 years ago
cinnaboot	a18cf925aa	add test case for orbit determination	4 years ago
cinnaboot	cb1ac9ce8e	replace reused test variables with constants	4 years ago
cinnaboot	4be3569771	update struct names to consistant PascalCase style	4 years ago
cinnaboot	aa913b32bf	correct NOTE in orbit test case 4.2	4 years ago
cinnaboot	25447510e8	add tests for time of flight	4 years ago
cinnaboot	a5c0cfa65f	remove even more (NOTE:) markers for inline comments	4 years ago
cinnaboot	021414ce3f	remove some (NOTE:) markers for inline comments	4 years ago
cinnaboot	8fe8a783f7	update tests	4 years ago
cinnaboot	1923e7a296	add orbital period property, and test case	4 years ago
cinnaboot	11fc5fa5e6	make use of system_2body time_step property	4 years ago
cinnaboot	bc8f84a297	fix tests	5 years ago
cinnaboot	5c45c2d6cd	update function names in orbit.h to be consistent with style	5 years ago
cinnaboot	5038d71a26	fix orbit_test	5 years ago
=	fb1f93b825	add constructEllipseAE	5 years ago
cinnaboot	9b3137d27b	update demo to use correct orbit propagation	5 years ago
cinnaboot	8fd3acd5ee	add testing with Catch2 for orbit propagation	5 years ago
cinnaboot	fcc3c85254	add orbit tests and update Makefile	5 years ago

26 Commits (88f2de41a460c8d2e3e44090c5c61babdbe574d8)