Orbit determination of FedSat based on GPS receiver position solutions – first results
Enderle, Werner, Feng, Yanming, & Zhou, Ning (2003) Orbit determination of FedSat based on GPS receiver position solutions – first results. In 6th International Symposium of Satellite Navigation Technology and Applications, 22-25 July 2003, Melbourne, Australia.
On 14th December 2002, the Australian small satellite FedSat was launched with a Japanese HII-A rocket into an 800 km sun-synchronous orbit with an inclination of 98.6 degrees. One of the payloads is a dual frequency GPS BlackJack receiver from NASA Jet Propulsion Laboratory (JPL). This receiver provides a Position, Velocity and Time (PVT) solution and also raw measurements (code and carrier), which will be used in different ways for Precise Orbit Determination (POD), Orbit Determination (OD) based on GPS position solutions, 2-axis Attitude Determination (AD) and atmospheric experiments.
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|Item Type:||Conference Paper|
|Keywords:||GPS Orbit Determination, Orbit Determination, ONS, GNSS, Space Flight Dynamics|
|Subjects:||Australian and New Zealand Standard Research Classification > ENGINEERING (090000) > ELECTRICAL AND ELECTRONIC ENGINEERING (090600)|
|Divisions:||Past > QUT Faculties & Divisions > Faculty of Built Environment and Engineering|
|Copyright Owner:||Copyright 2003 (please consult author)|
|Deposited On:||11 Jun 2004|
|Last Modified:||29 Feb 2012 13:02|
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