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Development and control of a 3-axis stabilised platform /Bredenkamp, Adolf Friedrich Ludwig January 2007 (has links)
Thesis (MScIng)--University of Stellenbosch, 2007. / Bibliography. Also available via the Internet.
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Employ sensor fusion techniques for determining aircraft attitude and position informationJarrell, Jason A. January 2008 (has links)
Thesis (M.S.)--West Virginia University, 2008. / Title from document title page. Document formatted into pages; contains xii, 108, [9] p. : ill. (some col.). Includes abstract. Includes bibliographical references (p. 104-108).
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A method for field calibration of a gyroscope in an airborne gravimetry inertial stable platform /Daoudi, Amina, January 1900 (has links)
Thesis (M. Eng.)--Carleton University, 2001. / Includes bibliographical references p. (115-117). Also available in electronic format on the Internet.
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Development and control of a 3-axis stabilised platformBredenkamp, Adolf Friedrich Ludwig 03 1900 (has links)
Thesis (MScEng (Electrical and Electronic Engineering))--University of Stellenbosch, 2007. / The successful control of a three-degree-of-freedom gyroscope is presented for the
application of steering and stabilising a platform mounted underneath an airship.
The end goal is to stabilise a camera for earth observation purposes.
The development of the necessary electronics, sensors and actuators along with
the hardware and software to interface these components are presented. This include
DC drives, torque control systems for the gimbal motors and a speed control system
for the gyroscope as well as platform angle and angular rate sensors.
A mathematical model for the gyroscope, based on Euler's equations of motion,
is presented. Non-linear simulations are performed and compared to measurements
of the plant's behaviour to step torque commands to determine the parameters of
the gyroscope. Pole placement and LQR optimal control methods are considered in
the design of a MIMO controller to steer the platform in the elevation plane, along
with a PI controller to steer the platform in the azimuth plane. Ground tests display
the success of the steering controllers.
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Design considerations for the standardized INS software development computer system.Ciccolo, Arthur Charles January 1976 (has links)
Thesis. 1976. M.S.--Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. / Microfiche copy available in Archives and Aero. / Includes bibliographical references. / M.S.
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The Validation of Interactive Computer Simulation Programs for Predicting On-Task Competencies for Inertial Navigation System EquipmentHageman, Dwight C. (Dwight Conrad) 05 1900 (has links)
This study investigated the predictive value of time on-task and error scores on tests administered through Control Data Corporation PLATO interactive computer graphics simulation as predictors of errors and time on-task for inertial navigation system equipment operation. In addition, the correlation between simulated pass/fail error and time on-task scores, and subsequent pass/fail criteria using actual equipment was investigated.
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