{"id":"v001","input":{"gradient":"200 ft/NM","groundspeed":"120 kt"},"expect":{"result.vertical_speed.value":400.0,"result.angle.value":1.885253852180525,"ok":true},"source":"Independent Python implementation of the turn, gradient, glide, and pivotal-altitude relations in FAA-H-8083-3C and FAA-H-8083-16B (tools/vectors/gen_aviation.py)","sourceVersion":"FAA-H-8083-16B (2017)","tolerance":{"result.vertical_speed.value":{"abs":1e-06,"rel":1e-09},"result.angle.value":{"abs":1e-06,"rel":1e-09}}}
{"id":"v002","input":{"gradient":"300 ft/NM","groundspeed":"90 kt"},"expect":{"result.vertical_speed.value":450.0,"result.angle.value":2.8266064014033825,"ok":true},"source":"Independent Python implementation of the turn, gradient, glide, and pivotal-altitude relations in FAA-H-8083-3C and FAA-H-8083-16B (tools/vectors/gen_aviation.py)","sourceVersion":"FAA-H-8083-16B (2017)","tolerance":{"result.vertical_speed.value":{"abs":1e-06,"rel":1e-09},"result.angle.value":{"abs":1e-06,"rel":1e-09}}}
{"id":"v003","input":{"gradient":"425 ft/NM","groundspeed":"160 kt"},"expect":{"result.vertical_speed.value":1133.3333333333333,"result.angle.value":4.001094289869373,"ok":true},"source":"Independent Python implementation of the turn, gradient, glide, and pivotal-altitude relations in FAA-H-8083-3C and FAA-H-8083-16B (tools/vectors/gen_aviation.py)","sourceVersion":"FAA-H-8083-16B (2017)","tolerance":{"result.vertical_speed.value":{"abs":1e-06,"rel":1e-09},"result.angle.value":{"abs":1e-06,"rel":1e-09}}}
{"id":"v004","input":{"gradient":"152 ft/NM","groundspeed":"200 kt"},"expect":{"result.vertical_speed.value":506.6666666666667,"result.angle.value":1.4330113542979013,"ok":true},"source":"Independent Python implementation of the turn, gradient, glide, and pivotal-altitude relations in FAA-H-8083-3C and FAA-H-8083-16B (tools/vectors/gen_aviation.py)","sourceVersion":"FAA-H-8083-16B (2017)","tolerance":{"result.vertical_speed.value":{"abs":1e-06,"rel":1e-09},"result.angle.value":{"abs":1e-06,"rel":1e-09}}}
{"id":"v005","input":{"gradient":"500 ft/NM","groundspeed":"75 kt"},"expect":{"result.vertical_speed.value":625.0,"result.angle.value":4.704237067623307,"ok":true},"source":"Independent Python implementation of the turn, gradient, glide, and pivotal-altitude relations in FAA-H-8083-3C and FAA-H-8083-16B (tools/vectors/gen_aviation.py)","sourceVersion":"FAA-H-8083-16B (2017)","tolerance":{"result.vertical_speed.value":{"abs":1e-06,"rel":1e-09},"result.angle.value":{"abs":1e-06,"rel":1e-09}}}