@InProceedings{OrlandoKugaLope:1997:ReGeTe,
author = "Orlando, Valcir and Kuga, Helio Kuga and Lopes, Roberto Vieira da
Fonseca",
affiliation = "{Instituto Nacional de Pesquisas Espaciais (INPE)}",
title = "Reducing the Geopotential Tesseral Harmonic Effects on Autonomous
Longitude Drift Control of Sun-Synchronous Satellites",
year = "1997",
pages = "361--374",
organization = "Advances in the Astronautical Sciences.",
keywords = "ENGENHARIA E TECNOLOGIA ESPACIAL.",
abstract = "Within a cooperation framework between INPE (National 1nstitute
for Space Research of Brazil) and CNES (Centre National d'Etudes
Spatiales of France), a study of a method for autonomous longitude
phase drift control was carried out and applied to phased orbits.
Real and simulated outputs from the DIODE autonomous orbit
determination system, developed by CNES, were preliminarly used to
test the concept. A simplified parabolic model was considered for
the longitude phase drift (L'>Lo ) time evolution. The
coefficients of this model are estimated in real time, from
observations of the first time derivative of L'>Lo (say{"}'Lu),
which are computed from the navigator orbit estimates. By using
the coefficients estimates, the model is used in the control
procedure in order to evaluate the amplitude of orbit sem i-major
axis corrections and the maneuver execution time. The obtained
results were very promising showing the feasibility of the
autonomous control impIementation. In particular, this paper deals
with the reduction cf the oscil!ations caused by the Geopotential
tesseral harmonic on the observations of {"}'Lu in order to
improve the studied autonomous orbit control procedure. We started
from a revised issue of the Ustinov's theory for near circular
orbits. The fuI! equations for the tesseral harmonics
perturbations on the orbit sem i-major axis and inclination have
been simplified considering low altitude, near zero eccentricity
and near polar phased orbits.",
copyholder = "SID/SCD",
label = "10926",
language = "en",
volume = "95",
urlaccessdate = "20 maio 2024"
}