2021
DOI: 10.1002/navi.416
|View full text |Cite
|
Sign up to set email alerts
|

Precise real‐time navigation of LEO satellites using GNSS broadcast ephemerides

Abstract: The availability of orbit information with high precision and low latency is a key requirement for many Earth‐observation missions, predominantly in the field of radio occultation. Traditionally, precise orbit determination solutions of low‐Earth orbit (LEO) satellites are obtained offline on ground after downloading GNSS measurements and auxiliary spacecraft data to the processing center. The latency of this processing depends on the frequency of LEO downlink contacts and the availability of precise GNSS orbi… Show more

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
1
1
1
1

Citation Types

0
12
0

Year Published

2021
2021
2023
2023

Publication Types

Select...
5
3

Relationship

2
6

Authors

Journals

citations
Cited by 40 publications
(18 citation statements)
references
References 37 publications
0
12
0
Order By: Relevance
“…These hybrid solutions combine the best of both techniques, but they increase the time latency. On the other hand, a technique that has gained attention in recent years [99] is the use of precise GNSS algorithms with broadcast ephemerides. The GNSS-POD with broadcast ephemerides allows precise positioning without the need for complementary ground-tospace links, thus reducing the latency issue.…”
Section: B Precise Orbit Determinationmentioning
confidence: 99%
“…These hybrid solutions combine the best of both techniques, but they increase the time latency. On the other hand, a technique that has gained attention in recent years [99] is the use of precise GNSS algorithms with broadcast ephemerides. The GNSS-POD with broadcast ephemerides allows precise positioning without the need for complementary ground-tospace links, thus reducing the latency issue.…”
Section: B Precise Orbit Determinationmentioning
confidence: 99%
“…Spacecraft operated at lower altitudes and experiencing higher drag forces would typically require an increased level of empirical forces, which then reduces the dynamical constraints on the resulting orbit. Nevertheless, independent simulations of GNSS-based real-time navigation (Hauschild and Montenbruck 2021) suggest that a better than 0.1 mm/s along-track velocity accuracy can even be reached for spacecraft orbiting at down to 400 km altitude.…”
Section: Resultsmentioning
confidence: 99%
“…These advantages are likewise of interest for GNSS-based onboard navigation of LEO satellites, which largely relies on the use of un-augmented broadcast ephemerides. Notable benefits of Galileo for this application have been earlier predicted in a simulation study of Hauschild and Montenbruck (2021) but lack a practical confirmation so far. Using actual flight data from the Sentinel-6A satellite now allows to reliably demonstrate the feasibility of 1 dm (3D RMS) real-time navigation using joint GPS and Galileo observations and shows that GNSS offers a viable alternative to DORIS for real-time orbit determination of LEO satellites.…”
Section: Introductionmentioning
confidence: 90%
“…Data processing is done with RTNAV (Hauschild & Montenbruck, 2021;Montenbruck & Ramos-Bosch, 2008), a multi-GNSS-capable software for LEO satellite navigation in a simulated real-time mode. It is based on an extended Kalman filter (EKF), using pseudoranges and carrier phases as measurement input and a reduced-dynamics orbit model (Wu et al, 1991) for propagation of the satellite's state vector.…”
Section: Data Processingmentioning
confidence: 99%
“…GNSS has been well proven and established for orbit determination in LEO for many years. It has been shown previously that dual-frequency, multi-constellation GNSS orbit determination in LEO using a carrier-phase approach with a reduced dynamics orbit model and broadcast ephemerides can achieve standard deviations of around one decimeter without external augmentation data (Hauschild & Montenbruck, 2021).…”
mentioning
confidence: 99%