Thesis (Ph. D.)--Johns Hopkins University, 1898. / Biography. eContent provider-neutral record in process. Description based on print version record.

Thesis (Ph. D.)--Johns Hopkins University, 1898. / Biography. Also issued in print.

No description available.

Thesis (Ph. D.)--University of Texas at Austin, 2000. / Vita. Includes bibliographical references (leaves 165-189). Available also in a digital version from Dissertation Abstracts.

This thesis explains the methodologies that predict the trajectory and accuracy of an unguided, indirect-fire launched projectile in predicted fire. The trajectory is the path that a projectile travels to the impact point, while the accuracy is the measurement of the deviation of the impact point from the target. In addition, this thesis describes, the methodology for calculating the various factors such as drag and drift in the trajectory calculation. A three degree of freedom model will be compared to a five degree of freedom model. With an accurate trajectory prediction, it is possible to calculate the delivery accuracy in a predicted fire, which does not have cumulative error corrections associated with the registration or adjusted fire. The delivery accuracies that are considered in this thesis are; 1) Mean Point of Impact (MPI) that are related to aiming errors and 2) Precision errors that are related to the dispersion caused by ballistics effect. Finally, the trajectory and accuracy estimates are compared with NATO Armament Ballistics Kernel (NATO) and Joint Weapons Accuracy Model (JWAM) respectively, and the differences are of the order of 4 percent.

Inaug.--Diss.--Göttingen. / Lebenslauf. Includes bibliographical references (p. 6).

No description available.

Inaug.--Diss.--Göttingen. / Lebenslauf. Includes bibliographical references (p. 6).

ITC/USA 2007 Conference Proceedings / The Forty-Third Annual International Telemetering Conference and Technical Exhibition / October 22-25, 2007 / Riviera Hotel & Convention Center, Las Vegas, Nevada / The US ARMY, ARDEC; in cooperation with AMCOM AMRDEC, Missile Guidance and Engineering Directorates; the Office of Naval Research; Naval Surface Fire Support; and the Naval Surface Weapon Center, requires multiphase development of a common, low-cost, high G survivable, high accuracy, Micro Electro-Mechanical Systems (MEMS) Inertial Measurement Unit (IMU) and Common, Deeply Integrated, Guidance and Navigation Unit (DI-GNU) for DoD gun launched guided munition and missile applications. The challenge for the Precision Munition Instrumentation Division (PMID) was to develop a Telemetry System to record the interior and exterior ballistics of a M831 TP-T projectile, which will be used as a carrier for soft recovery testing of IMUs and GNUs. This valuable data that would help The Government and contractors develop and validate multiple MEMS IMU design efforts, culminating with live fire verification performance test of pre-production in the Army’s 155-mm Soft Recovery Vehicle (SRVs) and missiles airframes.

Thesis (M.A.)--Texas State University-San Marcos, 2007. / Vita. Appendix: leaves 113-114. Includes bibliographical references (leaves 115-118).