Integrated Testing of the Cassini Saturn Orbit Insertion Critical Sequence

Cervantes, Daniel; Badaruddin, Kareem S.; Huh, Shin M.

doi:10.2514/6.2005-6272

Cited by 8 publications

(2 citation statements)

References 3 publications

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“…Several papers have been written on SOI and the efforts in FSW development and testing. [17][18] SOI successfully occurred on 30 June 2004.…”

Section: A Post-launch Fsw Development Methodologymentioning

confidence: 99%

“…An abundance of additional testing was focused on the critical events of SOI and Probe Relay. 10,[17][18][19] To support the prime mission, parameter and uplink procedure testing continued under the same test philosophy. During the prime mission, key science objectives were tested extensively which included post-event reconstruction i.e., Titan low-altitude flybys, 20 and low-altitude Enceladus flybys.…”

Section: B Post-launch Fsw Test Methodologymentioning

confidence: 99%

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Cassini Attitude Control Flight Software: From Development to In-Flight Operation

Brown

2008

AIAA Guidance, Navigation and Control Conference and Exhibit

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The Cassini Attitude and Articulation Control Subsystem (AACS) Flight Software (FSW) has achieved its intended design goals by successfully guiding and controlling the Cassini-Huygens planetary mission to Saturn and its moons. This paper describes an overview of AACS FSW details from early design, development, implementation, and test to its fruition of operating and maintaining spacecraft control over an eleven year prime mission. Starting from phases of FSW development, topics expand to FSW development methodology, achievements utilizing in-flight autonomy, and summarize lessons learned during flight operations which can be useful to FSW in current and future spacecraft missions.

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“…Several papers have been written on SOI and the efforts in FSW development and testing. [17][18] SOI successfully occurred on 30 June 2004.…”

Section: A Post-launch Fsw Development Methodologymentioning

confidence: 99%