Results 201 to 210 of about 939,430 (229)
NanoArduSiPM: A Miniaturized Integrated Platform for Scalable Scintillation-Based Particle Detection. [PDF]
Sensors (Basel)Bocci V +11 more
europepmc +1 more source
A Decoupled Doppler Positioning Algorithm for Dynamic Receivers Using LEO Constellation Signals. [PDF]
Sensors (Basel)Liu T +6 more
europepmc +1 more source
Hybrid Physics-Informed Residual Learning for Robust BDS-3 Satellite Clock Bias Prediction. [PDF]
Sensors (Basel)Cheng L +5 more
europepmc +1 more source
Different Behavior of Density Perturbations Between Dayside and Nightside in the Martian Thermosphere and the Ionosphere Associated With Atmospheric Gravity Waves. [PDF]
J Geophys Res Space PhysNakagawa H +8 more
europepmc +1 more source
Satellite onboard orbit propagation using Deprit’s radial intermediary
Celestial Mechanics and Dynamical Astronomy, 2014 Short-term satellite onboard orbit propagation is required when GPS position measurements are unavailable due to an obstruction or a malfunction. In this paper, it is shown that natural intermediary orbits of the main problem provide a useful alternative for the implementation of short-term onboard orbit propagators instead of direct numerical ...
Martin Lara, Pini Gurfil
exaly +5 more sources
Real-time onboard orbit propagator for planetary missions
AstrodynamicsDeveloping autonomous navigation systems for orbital platforms represents a frontier challenge in solar system exploration. A crucial element of such systems is the orbital propagator, which must accurately predict the spacecraft trajectory. Over short time scales, accurate state propagation is essential for processing data from onboard sensors within ...
Antonio Genova +2 more
exaly +4 more sources
Power savings through onboard orbit propagation for small satellites like NPSAT1 [PDF]
, 2016 Lieutenant, United States ...
Hartmann, David R.
core +4 more sources
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2014
The aim of this thesis will be modelling of the Rosetta spacecraft, including its relevant parts within Consert Unit and Philae Lander. For realize this subject, Feko code has been used, which is based on Method of Moments to determine radiation coupling effects and secondary propagation paths.
openaire +1 more source
The aim of this thesis will be modelling of the Rosetta spacecraft, including its relevant parts within Consert Unit and Philae Lander. For realize this subject, Feko code has been used, which is based on Method of Moments to determine radiation coupling effects and secondary propagation paths.
openaire +1 more source