@InProceedings{RaoLope:1995:FiExFi,
author = "Rao, K. R. and Lopes, Roberto Vieira da Fonseca",
title = "Satellite attitude follow-up: a first-hand experience with the
first Brazilian satellite SCD-1",
booktitle = "Proceedings...",
year = "1995",
pages = "777--783",
organization = "International Symposium on Space Dynamics.",
keywords = "ENGENHARIA E TECNOLOGIA ESPACIAL, Brazilian satellite, SCDI,
Complete Brazilian Space Mission (MECB), spin-axis, attitude
monitoring.",
abstract = "The first Brazilian satellite SCDI, designed and manufactured by
the Instituto Nacional de Pesquisas Espaciais - INPE under the
Complete Brazilian Space Mission (MECB) project, was launched on
February 09, 1993 at 14:42:20 UTC by a Pegasus rocket of Orbital
Sciences Corporation of USA. It is a spin-stabilized satellite and
its thermal constraints prohibit the orientation of the spin-axis
with respect to Sun's direction to rise above 90 degrees. Due to
this condition, some type of spin-axis attitude monitoring was
necessary during the useful lifetime of the satellite. Although
various types of algorithms were developed for this purpose,
unexpectedly, a software, which was developed during the
satellite's mission analysis phase mainly in order to furnish the
miss ion analysts with a fast, clear and integrated visualization
of the preliminary attitude determination results and related
aspects, was found useful for this purpose. For each orbit during
a specified period, this software prepares and draws on a computer
terminal, or optionally on a plotter, in inertial celestial sphere
containing: the Sun's position; the Earth's shadow; the
geomagnetic field vector trajectory; the satellite trajectory
during its pass over a given ground station; and the attitude of
the satellite spin-axis enveloped by its predicted uncertainty
ellipse. A rational analysis of this map helps a mission analyst
to select an optimum sub-set of satellite passes in order to
achieve the best possible precision in the attitude determination
process. However, besides fulfilling this main objective, after
the SCD1 launch. the attitude determination software was found to
be useful for various other purposes such as: the study of
magnetometer bias fluctuations, observed from one pass of the
satellite to other; an easy-monitoring of the spin-axis attitude
etc. This software also helped the mission analysts to take some
important decisions in improving the main attitude determination
software. This paper narrates everything about the attitude
follow-up software, starting from the initial idea based on which
the software was developed till the developments along time and
its final function. Being a debut of the attitude team of the
flight mechanics group of INPE, the experience with SCDI related
to attitude determination process gave challenging problems as
well as pleasant surprises, some of which are from the attitude
follow-up software. The main idea of this work is to share our
first-hand experience with the first Brazilian satellite SCD I in
the process of its attitude follow-up.",
conference-location = "Toulouse, FR",
conference-year = "19-23 June 1995",
label = "10928",
targetfile = "rama_satellite.pdf",
urlaccessdate = "04 maio 2024"
}