A series of three computer programs for the mathematical analysis of navigation and guidance of lunar and interplanetary trajectories was developed. All three programs require the integration of n-body trajectories for both interplanetary and lunar missions. The virutal mass technique is used in all three programs. The user's manual contains the information necessary to operate the programs. The input and output quantities of the programs are described. Sample cases are given and discussed.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Simulated trajectories error analysis program, version 2. Volume 2: Programmer's manual


    Contributors:

    Publication date :

    1971-03-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English


    Keywords :