Assessment of per-axis thruster control authority of cassini spacecraft for low-altitude titan flybys

Advances in the Astronautical Sciences

Volumn 119, Issue SUPPL., 2005, Pages 2743-2765

  Sarani, Siamak ^a,b  

^a CALIFORNIA INSTITUTE OF TECHNOLOGY   (United States)

^b Avionics System Engineering Section   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

FLYBYS; LAUNCH VEHICLES; ORBITER; THRUSTER CONTROL; LAUNCHING VEHICLES; RADIOISOTOPE THERMAL GENERATORS (RTG); REACTION WHEELS; THRUSTERS;

BOOSTERS (ROCKET); FLIGHT DYNAMICS; MATHEMATICAL MODELS; SATELLITES; SPACE PROBES; SPACECRAFT; TORQUE; TRAJECTORIES; ATMOSPHERIC DENSITY; CONTROL SYSTEMS; LAUNCHING; REMOTE SENSING; ROCKET ENGINES; SOLAR SYSTEM; SPACE FLIGHT; TORQUE MEASUREMENT;

ASTROPHYSICS; INTERPLANETARY SPACECRAFT;

EID: 23844474786     PISSN: 00653438     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (17)

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