Real-time navigation during the final approach phase of an interplanetary mission can significantly increase the accuracy of aerocapture and pin-point landing. The Mars Network is a versatile telecommunications network that is ideally situated to provide spacecraft-to-spacecraft radiometric navigation during Mars final approach and entry, descent, and landing via the Electra UHF transceiver, which is capable of providing autonomous, on-orbit, real-time trajectory determination using two-way Doppler measurements between a Mars approach vehicle and a Mars Network orbiter. A detailed dynamic analysis and link analysis of the final approach problem is presented, which seeks to determine the expected operating conditions of the Electra transceiver. In particular, the maximum Doppler shift and Doppler rate, which determine the transceiver tracking loop requirements, and the total received signal power and signal-to-noise ratio, which determine the range at which the communications link can be closed, are investigated for a range of Mars Network orbital geometries. A model of the Electra signal is developed on the basis of the results of the dynamic analysis and link analysis and is used as input to a high-fidelity simulation of the Electra transceiver. A Monte Carlo analysis is performed to determine the performance of the Electra transceiver for a range of signal and tracking loop parameters. In particular, the performance analysis focuses on the maximum range at which the link can be closed and on the acquisition and tracking performance of the second-order tracking loop. The analysis of the tracking performance is used to characterize and model the error in the Doppler measurement of the Electra transceiver. The error model is incorporated into the design of an extended Kalman filter, in order to improve the fidelity of the navigation filter design. The information content in the Doppler measurement and the observability of the estimated states are investigated for various orbital geometries and the accuracy of the navigation solution is analyzed.

published_or_final_version / Architecture / Master / Master of Architecture

Thesis (Ph. D.)--University of Texas at Austin, 2007. / Vita. Includes bibliographical references.

Thesis (M.S.)--Missouri University of Science and Technology, 2008. / Vita. The entire thesis text is included in file. Title from title screen of thesis/dissertation PDF file (viewed April 18, 2008) Includes bibliographical references (p. 127-129).

Thesis (M.S.)--University of Missouri-Columbia, 2003. / Accompany CD-ROM contains complete dissertation in Microsoft Word documents. Typescript. Vita. Includes bibliographical references. Also available on the Internet.

Thesis (M.S. in Space Systems Operations)--Naval Postgraduate School, September 2002. / Thesis advisor(s): Stephen A. Whitmore, Michael G. Spencer. Includes bibliographical references (p. 73-74). Also available online.

Thesis (M.M.A.S.)--School of Advanced Airpower Studies, 1995. / Subject: Cheap access to space. Cover page date: [1995]. Vita. Includes bibliographical references.

Thesis (M.S.)--University of Missouri-Columbia, 2003. / Accompany CD-ROM contains complete dissertation in Microsoft Word documents. Typescript. Vita. Includes bibliographical references. Also available on the Internet.

Thesis (M.S. in Astronautical Engineering)--Naval Postgraduate School, March 2005. / Thesis Advisor(s): I. Michael Ross. Includes bibliographical references (p. 57-58). Also available online.

While many studies have shown harmful effects of space flight on many tissues and systems of the human body, few studies have been done on the effects of space flight on the reproductive system. While the microgravity conditions of space flight are common knowledge, there is another component of space flight, that being higher than ambient (on Earth) levels of radiation. The purpose of this study was to examine the effects of simulated space flight on follicular development in the ovaries of mice, and to determine which component of spaceflight, i.e. microgravity, radiation, or a combination of the two, might be responsible for any changes in this follicular development. To simulate the environment of space, mice were exposed to higher levels of radiation by the use of cobalt plates and to simulated microgravity using a technique known as hind limb unloading. Four groups of mice-were used in this study; a control or untreated group, a group exposed to higher levels of radiation, a group exposed to simulated microgravity, and a group treated in both high radiation and simulated microgravity. The mice were further subdivided within these groups based on the amount of time they were kept alive after treatment/exposure (one, four, and nine months). The ovarian tissues were then analyzed to see the effects of these simulated conditions on the development of follicles. In all three treatment groups, development of follicles was restricted compared to the control group. Follicles from the various treatment groups appeared to be in the early stages of their development. It should be noted that these are preliminary results as the study is still in progress. One of the overarching questions that has been put forth by NASA over the last few decades is, can an organism, in this case a mammalian organism, complete an entire life cycle in space? This study may help to answer some of that question. If any of the components of space flight proves to be harmful to the female reproductive tissues human colonization of space would be problematic. If the damage incurred during space flight is irreversible, colonization of other worlds would also be problematic.