Spelling suggestions: "subject:"avigation systems"" "subject:"aavigation systems""
1 |
An analysis of transit and GPS point positioning resultsAbdalla, K. A. January 1987 (has links)
No description available.
|
2 |
Loran-C coverage prediction in Western EuropeFarnworth, Richard George January 1992 (has links)
No description available.
|
3 |
A study of the effects of stochastic inertial sensor errors in dead-reckoning navigationWall, John H. January 2007 (has links) (PDF)
Thesis (M.S.)--Auburn University, 2007. / Abstract. Includes bibliographic references (ℓ. 114-116)
|
4 |
Availability, continuity, and selection of maritime DGNSS radiobeaconsGrant, Alan James January 2002 (has links)
No description available.
|
5 |
A new technique for calibrating strapdown inertial reference units with large errors.Musoff, Howard January 1979 (has links)
Thesis (Sc.D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1979. / MICROFICHE COPY AVAILABLE IN ARCHIVES AND AERONAUTICS. / Includes bibliographical references. / Sc.D.
|
6 |
Drift performance vs. operating temperature in a low-cost strapdown gyroscope.Guerrero, Miguel Vicente January 1977 (has links)
Thesis. 1977. M.S.--Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. / MICROFICHE COPY AVAILABLE IN ARCHIVES AND AERONAUTICS. / Includes bibliographical references. / M.S.
|
7 |
Data fusion methodologies for multisensor aircraft navigation systemsJia, Huamin 04 1900 (has links)
The thesis covers data fusion for aircraft navigation systems in distributed sensor
systems. Data fusion methodologies are developed for the design, development,
analysis and simulation of multisensor aircraft navigation systems. The problems of
sensor failure detection and isolation (FDI), distributed data fusion algorithms and
inertial state integrity monitoring in inertial network systems are studied.
Various existing integrated navigation systems and Kalman filter architectures are
reviewed and a new generalised multisensor data fusion model is presented for the
design and development of multisensor navigation systems. Normalised navigation
algorithms are described for data fusion filter design of inertial network systems.
A normalised measurement model of skewed redundant inertial measurement units
(SRIMU) is presented and performance criteria are developed to evaluate optimal
configurations of SRIMUs in terms of the measurement accuracy and FDI capability.
Novel sensor error compensation filters are designed for the correction of SRIMU
measurement errors. Generalised likelihood ratio test (GLRT) methods are improved
to detect various failure modes, including short time and sequential moving-window
GLRT algorithms.
State-identical and state-associated fusion algorithms are developed for two forms of
distributed sensor network systems. In particular, innovative inertial network sensing
models and inertial network fusion algorithms are developed to provide estimates of
inertial vector states and similar node states. Fusion filter-based integrity monitoring
algorithms are also presented to detect network sensor failures and to examine the
consistency of node state estimates in the inertial network system.
The FDI and data fusion algorithms developed in this thesis are tested and their
performance is evaluated using a multisensor software simulation system developed
during this study programme. The moving-window GLRT algorithms for optimal
SRIMU configurations are shown to perform well and are also able to detect jump
and drift failures in an inertial network system. It is concluded that the inertial
network fusion algorithms could be used in a low-cost inertial network system and
are capable of correctly estimating the inertial vector states and the node states.
|
8 |
Moving base INS/GPS vector gravimetry on a land vehicleLi, Xiaopeng , January 2007 (has links)
Thesis (Ph. D.)--Ohio State University, 2007. / Title from first page of PDF file. Includes bibliographical references (p. 162-170).
|
9 |
Integration of local area augmentation system and inertial navigation system for aircraft surface movement guidanceMarti, Lukas Michael. January 2000 (has links)
Thesis (M.S.)--Ohio University, August, 2000. / Title from PDF t.p.
|
10 |
Initial characterization of QBIC IMU and design of a DATAC bus interfaceMathur, Navin G. January 1993 (has links)
Thesis (M.S.)--Ohio University, November, 1993. / Title from PDF t.p.
|
Page generated in 0.1157 seconds