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Oliver Montenbruck

Researcher at German Aerospace Center

Publications -  255
Citations -  11077

Oliver Montenbruck is an academic researcher from German Aerospace Center. The author has contributed to research in topics: Global Positioning System & GNSS applications. The author has an hindex of 46, co-authored 242 publications receiving 9089 citations.

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Book

Satellite Orbits: Models, Methods and Applications

TL;DR: This is a modern textbook that guides the reader trough the theory and practice of satellite orbit prediction and determination from basic principles of orbital mechanics, and covers elaborate force models as well as precise methods of satellite tracking.
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The Multi-GNSS Experiment (MGEX) of the International GNSS Service (IGS) - Achievements, prospects and challenges

TL;DR: The status and tracking capabilities of the IGS monitoring station network are presented and the multi-GNSS products derived from this resource are discussed and the achieved performance is assessed and related to the current level of space segment and user equipment characterization.
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Springer Handbook of Global Navigation Satellite Systems

TL;DR: In this article, the authors present a complete and rigorous overview of the fundamentals, methods and applications of the multidisciplinary field of Global Navigation Satellite Systems (GNSS), providing an exhaustive, one-stop reference work and a state-of-the-art description of GNSS as a key technology for science and society at large.
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Initial assessment of the COMPASS/BeiDou-2 regional navigation satellite system

TL;DR: An initial characterization and performance assessment of the COMPASS/BeiDou-2 regional navigation system is presented and the benefit of triple-frequency measurements and extra-wide-lane ambiguity resolution is illustrated for relative positioning on a short baseline.
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Proximity Operations of Formation-Flying Spacecraft Using an Eccentricity/Inclination Vector Separation

TL;DR: In this paper, an elegant formulation of the linearized equations of relative motion is discussed and adopted for satellite formation design, and the concept of eccentricity/inclination-vector separation is extended to low-Earth-orbit (LEO) formations.