A generalized mission design scheme which utilizes a standard mission profile for all OMV rendezvous operations, recognizes typical operational constraints, and minimizes propellant penalties due to nodal regression effects was developed. This scheme has been used to demonstrate a unified guidance and navigation maneuver processor (the UMP), which supports all mission phases through station-keeping. The initial demonstration version of the Orbital Rendezvous Mission Planner (ORMP) was provided for evaluation purposes, and program operation was discussed.
Automatic Rendezvous and Docking Systems Functional and Performance Requirements
1985
16 pages
Report
No indication
English
Automatic Rendezvous and Docking Final Report
NTIS | 1970
|Automatic rendezvous and docking Final report
NTRS | 1970
|British Library Online Contents | 1996
|Springer Verlag | 2008
|