An overall parametric system analysis of the use of an optical approach guidance measurement system (using a V-slit electrooptical 'star-pipper') onboard a Pioneer-type spin-stabilized spacecraft for outer planet missions. Optical measurements of satellites of Saturn and Uranus against the star background are considered. Measurement geometry and spacecraft attitude are evaluated in depth with respect to two Pioneer missions: Saturn-Uranus and Jupiter-Uranus atmospheric entry probe missions with departure from Earth in November/December, 1980. A preliminary evaluation of long-term attitude stability measurements of Pioneer 10 is presented in the Appendix. The major conclusions are: (1) at Saturn flyby, viewing some medium period satellites can provide the best measurement results. (2) At Uranus approach, viewing the planet may give best measurements if early bus-probe separation is required. (3) Final measurement accuracy depends on the data format transmitted to Earth and the applied data interpretation techniques.-
Approach guidance for outer planet Pioneer missions
International Astronautical Federation, International Astronautical Congress ; 1974 ; Amsterdam, Netherlands
1974-09-01
Conference paper
No indication
English
Approach guidance for outer planet pioneer missions
NTRS | 1975
|Approach Guidance for Outer Planet Pioneer Missions
NTIS | 1975
|Unmanned outer planet capture missions.
NTRS | 1969
|Unmanned outer planet capture missions.
AIAA | 1969
|