Comet 19P/Borrelly orbit determination for the DS1 flyby
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Engineering topics
Publications and source records attributed to Bhaskaran, S..
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This paper presents covariance studies showing that the radio data can produce entry accuracies better than 0.1 degrees in flight-path angle and better than one km in position.
NASA's New Millenium Program consists of a series of missions whose primary purpose is to demonstrate the feasibility of new technologies for space flight.
Deep Space 1 is the first mission in NASA's New Millennium Program, a series of missions to demonstrate the feasibility of new technologies for spaceflight.
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The first mission of NASA's New Millennium Program, Deep Space 1, has, as one of its principal demonstration-technologies, the first autonomous optical navigation system to be used in deep space.
The first mission of NASA's New Millenium Program, Deep Space 1, has, as one of its principal demonstration technologies, the first autonomous optical navigation system to be used in deep space.
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NASA's New Millennium Program involves a series of missions whose primary purpose is to demonstrate the feasibility of new technologies for spaceflight.
STARDUST is a mission to flyby the comet Wild-2 in early 2004 and return samples of the coma to Earth.
The autonomous optical navigation system technology for the Deep Space 1 (DS1) mission is reported on. The DS1 navigation system will be the first to use autonomous navigation in deep space. The systems tasks are to: perform interplanetary cruise orbit determination using images of distant asteroids; control and maintain the orbit of the spacecraft with an ion propulsion system and conventional thrusters, and perform late knowledge updates of target position during close flybys in order to facilitate high quality data return from asteroid MaAuliffe and comet West-Kohoutek-Ikemura. To accomplish these tasks, the following functions are required: picture planning; image processing; dynamical modeling and integration; planetary ephemeris and star catalog handling; orbit determination; data filtering and estimation; maneuver estimation, and spacecraft ephemeris updating. These systems and functions are described and preliminary performance data are presented.
This paper summarizes Galileo's orbit determination activities leading up to its encounter with asteroid 243-Ida on August 28, 1993. In addition to the nominal 2-way S-band range and Doppler radio metric data obtained from the Deep Space Network (DSN), several navigational aids were brought together to make this encounter successful.
The first flight of NASA's New Millennium Program, Deep Space-1, will include a new navigational technology: a fully autonomous optical navigation system.
The automation of interplanetary spacecraft is becoming increasingly desirable to meet various mission requirements. A prototype of an autonomous spacecraft which will fly by an asteroid and comet is slated for flight in mid-1998 as part of NASA's New Millenium Program.
The first fully autonomous deep-space navigation system ever implemented is planned to guide the New Millenium Deep Space-1 mission to an asteroid and comet beginning in mid-1998. This system is based to a large extent on Optical Navigation (OPNAV) technology developed for the NASA/JPL interplanetary exploration probes Voyager and Galileo. This paper describes the structure and algorithmic content of the Autonomous OPNAV system. The system has several major autonomous functions: picture planning, image analysis, orbit determination, manuever design and general interaction with other onboard autonomous systems.
An algorithm is described and demonstrated with a simulation that has been developed for navigation around small bodies. This is important because of the cost and complexity of using ground control for navigating around such objects. The algorithm uses a precomputed shape model of the object and images taken with a wide field-of-view (FOV) camera.
This paper presents an algorithm to autonomously determine the orbit of a spacecraft around a small solar system object (such as an asteroid) using a wide field-of-view camera and a precomputed model of the object.