Development of a GPS-aided inertial platform for an airborne scalar gravity system

Simple item page
dc.contributor.advisorSchwarz, Klaus-Peter P.
dc.contributor.authorZhang, Qiyue John
dc.date.accessioned2005-07-29T22:09:21Z
dc.date.available2005-07-29T22:09:21Z
dc.date.issued1995
dc.descriptionBibliography: p. 115-124en
dc.description.abstractThe development of a OPS-aided inertial platform for an airborne scalar gravity system is described in this dissertation. Damping Schuler oscillations of an airborne inertial platform and achieving a levelling accuracy of a few arc seconds are the main objectives. System errors are analyzed and modelled. Two methods for inertial platform levelling loop stabilization by OPS velocity are analysed and compared, one using an open loop design, the other a closed loop design. Algorithms for platform initial alignment, gyro drift and navigation, which are fundamental to the OPS-aided inertial platform, have been designed and implemented. A series of tests on kinematic double difference OPS position and velocity errors have been performed using a precise positioning stage as a reference. A radio data link system is designed to eliminate Selective Availability (SA) effects on real-time OPS velocity. Accuracy and time latency of the real-time DOPS system are tested. To evaluate algorithms and methods, platform systems are simulated, and both methods of platform stabilization are applied to flight data taken by the ITC-2 inertial platform and a set of Trimble 4000 SSE receivers on board of a Cessna 310 twin engine air plane. Both theoretical analysis and results of simulation and flight test indicate that the Schuler oscillations of an inertial platform can be damped by OPS velocity to an accuracy of a few arc seconds and that the platform levelling accuracy can thus be significantly improved.En
dc.format.extentxvi, 124 leaves : ill. ; 30 cm.en
dc.identifier.citationZhang, Q. J. (1995). Development of a GPS-aided inertial platform for an airborne scalar gravity system (Doctoral thesis, University of Calgary, Calgary, Canada). Retrieved from https://prism.ucalgary.ca. doi:10.11575/PRISM/13969en_US
dc.identifier.doihttp://dx.doi.org/10.11575/PRISM/13969
dc.identifier.isbn0612042073en
dc.identifier.lccQB 331 Z53 1995en
dc.identifier.urihttp://hdl.handle.net/1880/29778
dc.language.isoeng
dc.publisher.institutionUniversity of Calgaryen
dc.publisher.placeCalgaryen
dc.rightsUniversity of Calgary graduate students retain copyright ownership and moral rights for their thesis. You may use this material in any way that is permitted by the Copyright Act or through licensing that has been assigned to the document. For uses that are not allowable under copyright legislation or licensing, you are required to seek permission.
dc.subject.lccQB 331 Z53 1995en
dc.subject.lcshGravimeters (Geophysical instruments)
dc.subject.lcshInertial navigation systems
dc.subject.lcshGlobal positioning system
dc.titleDevelopment of a GPS-aided inertial platform for an airborne scalar gravity system
dc.typedoctoral thesis
thesis.degree.disciplineGeomatics Engineering
thesis.degree.grantorUniversity of Calgary
thesis.degree.nameDoctor of Philosophy (PhD)
ucalgary.item.requestcopytrue
ucalgary.thesis.accessionTheses Collection 58.002:Box 1012 520538322
ucalgary.thesis.notesoffsiteen
ucalgary.thesis.uarcreleaseyen
Files
Original bundle
Now showing 1 - 1 of 1
Thumbnail Image
Name:
thesis_Zhang_1995.pdf
Size:
48.61 MB
Format:
Adobe Portable Document Format
Description:
Download
Collections
Legacy Theses