✦ LIBER ✦

Accounting of fundamental components of the rotation parameters of the Earth in the formation of a high-accuracy orbit of navigation satellites

✍ Scribed by Yu. G. Markov, M. V. Mikhailov, V. N. Pochukaev

Book ID: 119883783
Publisher: SP MAIK Nauka/Interperiodica
Year: 2012
Tongue: English
Weight: 266 KB
Volume: 57
Category: Article
ISSN: 1028-3358
DOI: 10.1134/s1028335812070026

No coin nor oath required. For personal study only.

📜 SIMILAR VOLUMES

Fundamental components of parameters of

Fundamental components of parameters of the Earth’s rotation used to produce high-accuracy navigation systems for spacecraft

✍ Yu. G. Markov, M. V. Mikhailov, V. N. Pochukaev 📂 Article 📅 2013 🏛 SP MAIK Nauka/Interperiodica 🌐 English ⚖ 416 KB

The Effect of Atmospheric Rotation on th

The Effect of Atmospheric Rotation on the Orbital Plane of a Near-Earth Satellite

✍ Cook, G. E.; Plimmer, R. N. A. 📂 Article 📅 1960 🏛 The Royal Society 🌐 English ⚖ 615 KB

Biaxial Mode of Rotation of a Satellite

Biaxial Mode of Rotation of a Satellite in the Orbit Plane

✍ V. I. Vetlov; S. M. Novichkova; V. V. Sazonov; S. Yu. Chebukov 📂 Article 📅 2000 🏛 Springer 🌐 English ⚖ 344 KB

The relativistic equations of motion for

The relativistic equations of motion for a satellite in orbit about a finite-size, rotating Earth

✍ Mark A. Vincent 📂 Article 📅 1986 🏛 Springer Netherlands 🌐 English ⚖ 453 KB

Improvement in the orbital parameters of

Improvement in the orbital parameters of GLONASS navigation satellites based on non-interrogatory measurements of pseudodistances

✍ A. Ya. Yudanin; B. S. Mogilnitskii; A. S. Tolstikov 📂 Article 📅 2009 🏛 Springer US 🌐 English ⚖ 148 KB

The component of the earth's orbital vel

The component of the earth's orbital velocity in a given line of sight

✍ Dr. Frank Schlesinger 📂 Article 📅 1899 🏛 John Wiley and Sons 🌐 English ⚖ 99 KB 👁 2 views

In observations for motions in the line of sight it is necessary to make allowance for the observer's diurnal motion and also for the motion of the earth as a whole in its orbit. To compute the latter we tnay proceed as follows. Let