Sean V. Wagner
California Institute of Technology
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Featured researches published by Sean V. Wagner.
AIAA/AAS Astrodynamics Specialist Conference and Exhibit | 2006
Sean V. Wagner; Emily M. Gist; Troy Goodson; Yungsun Hahn; Paul W. Stumpf; Powtawche N. Williams
This paper documents the maneuver experience during the second year of the Cassini-Huygens mission at Saturn. Since Saturn arrival in July 2004, the Cassini orbiter has made many flybys of Titan and Saturns icy satellites. From August 2005 to June 2006, there were 39 planned maneuvers designed to target Cassini to aimpoints near Titan, Hyperion, Dione, and Rhea. Highlights of this paper include maneuver designs and strategies, maneuver performance, maneuver cancellation rationales, and a new maneuver execution-error model based on maneuvers executed to date.
AIAA/AAS Astrodynamics Specialist Conference | 2010
Christopher G. Ballard; Juan Arrieta; Yungsun Hahn; Paul W. Stumpf; Sean V. Wagner; Powtawche N. Williams
The Cassini-Huygens spacecraft was launched in 1997 on a mission to observe Saturn and its many moons. After a seven-year interplanetary cruise, it entered a Saturnian orbit for a four-year Prime Mission in 2004 and began a two-year Equinox Mission in 2008. It has been approved for another seven-year mission, the Solstice Mission, starting in October 2010. This paper highlights significant maneuver activities performed from July 2009 to June 2010. We present results for the 45 maneuvers during this time. The successful navigation of the Cassini orbiter can be attributed in part to the accurate maneuver performance, which has greatly exceeded pre-launch expectations.
SpaceOps 2008 Conference | 2008
Powtawche N. Williams; Emily M. Gist; Troy Goodson; Yungsun Hahn; Paul W. Stumpf; Sean V. Wagner
The Cassini-Huygens spacecraft was launched in 1997 as an international and collaborative mission to study Saturn and its many moons. After a seven-year cruise, Cassini began orbiting Saturn for a four- year tour. This tour consists of 157 planned maneuvers, and their back-up locations, designed to target 52 encounters, mostly of Saturns largest moon Titan. One of the missions first activities was to release the Huygens probe to Titan in December 2004. Currently in its last year of the prime mission, Cassini-Huygens continues to obtain valuable data on Saturn, Titan, and Saturns other satellites. Return of this information is in large part due to a healthy spacecraft and successful navigation. A two-year extended mission, beginning July 2008, will offer the opportunity to continue science activities. With a demanding navigation schedule that compares with the prime tour, the Cassini Navigation team relies on operations procedures developed during the prime mission to carry-out the extended mission objectives. Current processes for orbit control operations evolved from the primary navigational requirement of staying close to predetermined targeting conditions according to Cassini science sequence planning. The reference trajectory is comprised of flyby conditions to be accomplished at minimal propellant cost. Control of the planned reference trajectory orbit, and any trajectory updates, is achieved with the execution of Orbit Trim Maneuvers (OTMs). The procedures for designing, processing, and analyzing OTMs during Cassini operations is presented. First, a brief overview of the Cassini-Huygens Mission is given, followed by a general description of navigation. Orbit control and maneuver execution methods are defined, along with an outline of the orbit control staffing and operations philosophy. Finally, an example schedule of orbit control operations is shown.
AIAA/AAS Astrodynamics Specialist Conference | 2012
Sean V. Wagner; Juan Arrieta; Christopher G. Ballard; Yungsun Hahn; Paul W. Stumpf; Powtawche N. Valerino
The Solstice Mission is the final extension of the Cassini spacecraft s tour of Saturn and its moons. To accommodate an end-of-mission in 2017, the maneuver decision process has been refined. For example, the Cassini Project now prioritizes saving propellant over minimizing maneuver cycles. This paper highlights 30 maneuvers planned from June 2012 through July 2013, targeted to nine Titan flybys and the final Rhea encounter in the mission. Of these maneuvers, 90% were performed to maintain the prescribed trajectory and preserve downstream delta V. Recent operational changes to maneuver executions based on execution-error modeling and analysis are also discussed.
AIAA/AAS Astrodynamics Specialist Conference and Exhibit | 2008
Troy Goodson; Christopher G. Ballard; Emily M. Gist; Yungsun Hahn; Paul W. Stumpf; Sean V. Wagner; Powtawche N. Williams
The Cassini-Huygens spacecraft was launched in 1997 on a mission to observe Saturn and its many moons. After a seven-year cruise, it entered a Saturnian orbit for a four-year, prime mission. This paper highlights significant maneuver activities performed during the last year of the prime mission. Specifically, results of 42 recent maneuvers are presented. Many maneuvers have been skipped, saving fuel and flight team effort. The system has performed more accurately than the pre-launch expectations and requirements. This is in large part why the Cassini-Huygens spacecraft has been navigated with tremendous success during the prime mission.
AIAA/AAS Astrodynamics Specialist Conference and Exhibit | 2008
Sean V. Wagner; Emily M. Gist; Troy Goodson; Yungsun Hahn; Paul W. Stumpf; Powtawche N. Williams
The Cassini-Huygens Saturn tour poses an interesting navigation challenge. From July 2004 through June 2008, the Cassini orbiter performed 112 of 161 planned maneuvers. This demanding schedule, where maneuvers are often separated by just a few days, motivated the development of maneuver design/analysis automation software tools. Besides generating maneuver designs and presentations, these tools are the mechanism to producing other types of navigation information; information used to facilitate operational decisions on such issues as maneuver cancellation and alternate maneuver strategies. This paper will discuss the navigation data that are communicated inside the Cassini-Huygens Project, as well as the maneuver software tools behind the processing of the data.
AIAA/AAS Astrodynamics Specialist Conference | 2014
Mar Vaquero; Yungsun Hahn; Paul W. Stumpf; Powtawche N. Valerino; Sean V. Wagner; Mau Wong
After sixteen years of successful mission operations and invaluable scientific discoveries, the Cassini orbiter continues to tour Saturn on the most complex gravity-assist trajectory ever flown. To ensure that the end-of-mission target of September 2017 is achieved, propellant preservation is highly prioritized over maneuver cycle minimization. Thus, the maneuver decision process, which includes determining whether a maneuver is performed or canceled, designing a targeting strategy and selecting the engine for execution, is being continuously re-evaluated. This paper summarizes the maneuver experience throughout the fourth year of the Solstice Mission highlighting 27 maneuvers targeted to nine Titan flybys.
Archive | 2005
Troy Goodson; Brent Buffington; Yungsun Hahn; Nathan Strange; Sean V. Wagner; Mau Wong
Archive | 2009
Emily M. Gist; Christopher G. Ballard; Yungsun Hahn; Paul W. Stumpf; Sean V. Wagner; Powtawche N. Williams
Archive | 2006
Troy Goodson; Amy Attiyah; Brent Buffington; Yungsun Hahn; Joan Pojman; Bob Stavert; Nathan Strange; Paul W. Stumpf; Sean V. Wagner; Peter Wolff; Mau Wong