Results 61 to 70 of about 725 (134)
The high-precision satellite velocities and accelerations calculated by the Global Navigation Satellite System (GNSS) are essential for tasks such as airborne gravity data processing.
Chuanfeng Song +4 more
doaj +1 more source
Accurate and Rapid Broadcast Ephemerides for Beidou-Maneuvered Satellites
The geostationary earth orbit (GEO) and inclined geosynchronous orbit (IGSO) satellites of the Beidou navigation satellite system are maneuvered frequently. The broadcast ephemeris can be interrupted for several hours after the maneuver.
Jing Qiao +3 more
doaj +1 more source
Optical Photometry of LMXBs: UW CrB (=MS 1603+260) and V1408 Aql (=4U 1957+115)
We present new optical observations of V1408 Aql (= 4U 1957+115), the only low mass X-ray binary, black hole candidate known to be in a persistently soft state.
P. A. Mason +3 more
doaj +1 more source
Beginnings of Satellite Navigation
The first satellite navigation system called the Navy Navigation Satellite System (NNSS) or TRANSIT was planned in the USA in 1958. It consisted of 5-6 artificial Earth satellites, was set in motion for the USA military in 1964, and in 1967 for civilian ...
Miljenko Solarić
doaj
Study on the Design of Broadcast Ephemeris Parameters for Low Earth Orbit Satellites
The integration of low Earth orbit (LEO) satellite constellations into the Global Navigation Satellite System (GNSS) has emerged as a prominent research focus, as LEO satellites can significantly enhance the precision of GNSS positioning, navigation, and
Dongzhu Liu +4 more
doaj +1 more source
Image Positioning Accuracy Analysis for Super Low Altitude Remote Sensing Satellites
Super low altitude remote sensing satellites maintain lower flight altitudes by means of ion propulsion in order to improve image resolution and positioning accuracy.
Ming Xu, Nan Zhou
doaj +1 more source
Utilization CSRS-PPP software for recovery aircraft’s position [PDF]
The PPP method is applied in aeronautical navigation as a new technique for determination of aircraft’s position. In this paper preliminary results of recovery aircraft’s position were presented.
Kamil KRASUSKI
doaj
Realtime Precise Orbit Determination Technology for LEO Mega-Constellation
Supported by GNSS, it analyzed the advantages and disadvantages of solving LEO satellite orbit on the ground or onboard the satellites.The high-fidelity non-conservative force models were applied to the real-time orbit determination algorithm.To separate
Zhen LI, Chuang SHI
doaj +2 more sources
Cooperative Design of Ranging and Communication for In-Band Full-Duplex Inter-Satellite Links. [PDF]
Feng H +7 more
europepmc +1 more source
Observation Series-Based Skymask Establishment and NLOS Exclusion for Smartphone Positioning. [PDF]
Liu C, Wu K.
europepmc +1 more source

