Used to calculate the particle trajectory of spacecraft re-entry, including the interpolation algorithm, Runge-Kutta method as well as atmospheric model

Packet : 35738599zairuzhidiandandao.rar filelist
航天器再入质点弹道\AirModel.cpp
航天器再入质点弹道\AirModel.h
航天器再入质点弹道\Data_Cx_Vec.txt
航天器再入质点弹道\Data_Cy_Vec.txt
航天器再入质点弹道\Data_Dim.txt
航天器再入质点弹道\Debug
航天器再入质点弹道\Main.cpp
航天器再入质点弹道\Model.cpp
航天器再入质点弹道\Model.h
航天器再入质点弹道\result.txt
航天器再入质点弹道\插值.cpp
航天器再入质点弹道\插值.h
航天器再入质点弹道\数值积分.cpp
航天器再入质点弹道\数值积分.h
航天器再入质点弹道\航天器再入质点弹道.dsp
航天器再入质点弹道\航天器再入质点弹道.dsw
航天器再入质点弹道\航天器再入质点弹道.ncb
航天器再入质点弹道\航天器再入质点弹道.opt
航天器再入质点弹道\航天器再入质点弹道.plg
航天器再入质点弹道

• We are an exchange download platform that only provides communication channels. The downloaded content comes from the internet. Except for download issues, please Google on your own.
• The downloaded content is provided for members to upload. If it unintentionally infringes on your copyright, please contact us.
• Please use Winrar for decompression tools
• If download fail, Try it againg or Feedback to us.
• If downloaded content did not match the introduction, Feedback to us，Confirm and will be refund.
• Before downloading, you can inquire through the uploaded person information

Nothing．