The electrodynamics of the Earth's low-latitude ionosphere is dependent on the ionospheric conductivity and the thermospheric neutral density, temperature, and winds present. This two-part study focused on the gravity wave seeding mechanism of equatorial plasma depletions in the ionosphere and the associated equatorial spread F, as well as the differences between a two-dimensional flux tube integrated electrodynamics model and a three-dimensional model for the same time period. The gravity wave seeding study was based on a parameterization of a gravity wave perturbation using a background empirical thermosphere and a physics-based ionosphere for the case of 12 UT on 26 September 2002. The electrodynamics study utilized a two-dimensional flux tube integrated model in center dipole coordinates, which is derived in this work. This case study examined the relative influence of the zonal wind, meridional wind, vertical wind, temperature, and density perturbations of the gravity wave. It further looked at the angle of the wave front to the field line flux tube, the most influential height of the perturbation, and the difference between planar and thunderstorm source gravity waves with cylindrical symmetry. The results indicate that, of the five perturbation components studied, the zonal wind is the most important mechanism to seed the Rayleigh-Taylor instability needed to develop plasma plumes. It also shows that the bottomside of the F-region is the most important region to perturb, but a substantial E-region influence is also seen. Furthermore, a wave front with a small angle from the field line is necessary, but the shape of the wave front is not critical in the gravity wave is well developed before nightfall. Preliminary results from the three-dimensional model indicate that the equipotential field line assumption of the two-dimensional model is not valid below 100 km and possibly higher. Future work with this model should attempt to examine more of the differences with the two-dimensional model in the electric fields and currents produced as well as with the plasma drifts that lead to plume development.

L'ionosphère du côté nuit de Mars reste encore à ce jour une zone mystérieuse et peu connue de l'environnement Martien. Les déplétions d'électrons suprathermiques sont des structures spécifiques à cette région, observées jusqu'à présent par trois satellites : Mars Global Surveyor (MGS), Mars EXpress (MEX) et Mars Atmosphere and Volatile EvolutioN (MAVEN). Leur étude permet aussi bien l'observation de la structure et de la dynamique de l'ionosphère du côté nuit que celle de l'atmosphère neutre, de la topologie magnétique martienne, ainsi que l'étude de l'échappement atmosphérique de Mars. Des structures aussi différentes que les cornets magnétiques, les couches de courants ou encore le terminateur ultra-violet peuvent être examinées à travers les déplétions d'électrons suprathermiques, de par les mécanismes à l'origine de leur présence du côté nuit de Mars. Le but principal de ma thèse a été de tirer parties des trois jeux de données offerts par les satellites MGS, MEX et MAVEN pour mieux comprendre les mécanismes à l'origine des déplétions d'électrons suprathermiques observées du côté nuit ainsi que leur impact sur la structure et la dynamique de l'ionosphère du côté nuit. Dans cette optique, trois critères simples adaptés à chaque mission ont été développés pour identifier les déplétions d'électrons suprathermiques dans une base de données allant de 1999 à 2017. Une étude statistique a révélé la présence d'une région de transition autour de 170 km d'altitude séparant la région collisionnelle dans laquelle les déplétions d'électrons suprathermiques sont directement dues à l'absorption des électrons par le CO_2 atmosphérique, et la région non-collisionnelle dans laquelle elles sont principalement dues aux boucles fermées de champs magnétique d'origine crustale. La compréhension de ces mécanismes m'a permis d'estimer la localisation du terminateur ultra-violet. Celui-ci est situé en moyenne ~120 km au-dessus du terminateur optique. Cette altitude varie entre le côté soir et le côté matin, et une variation saisonnière est prédite par les modèles atmosphériques. / The nightside ionosphere of Mars still remains an unfamiliar and mysterious place. Nightside suprathermal electron depletions are specific features of this region which have been observed at Mars by three spacecraft to date: Mars Global Surveyor (MGS), Mars EXpress (MEX) and the Mars Atmosphere and Volatile EvolutioN (MAVEN) mission. Their study enables the observation of the nightside ionosphere structure and dynamics as well as the underlying neutral atmosphere, the specific Martian magnetic topology, and possible conduits for atmospheric escape. Structures as different as magnetic cusps, current sheets or the UV terminator can be investigated through suprathermal electron depletions, due to the processes leading to their observation on the nightside of Mars. The main goal of my PhD has been to use the complementarity of the three missions MGS, MEX, and MAVEN to understand the different mechanisms at the origin of suprathermal electron depletions and their implication on the structure and the dynamics of the nightside ionosphere. In this context, three simple criteria adapted to each mission have been implemented to identify suprathermal electron depletions from 1999 to 2017. A statistical study reveals a transition region near 170 km altitude separating the collisional region where suprathermal electron depletions are directly due to electron absorption by atmospheric CO_2 and the collisionless region where they are mainly due to electron exclusion by closed crustal magnetic field loops. Understanding of these phenomena enables me to estimate the location of the UV terminator. It appears to be located ~120 km above the optical terminator, though this location is different between the dawn and dusk terminator and is expected to vary throughout the different Martian seasons.

Satellites have revolutionized navigation by making it more universal, accessible and ac- curate. Global Positioning System (GPS) is the most widely used satellite navigation system in the world. However, it is prone to errors from various sources such as the ionosphere, troposphere and clock biases. In order to make the system very accurate and reliable, especially to meet the requirements of safety-critical applications, Satellite Based Augmentation Systems (SBAS) have recently been designed in various countries to augment the GPS by providing corrections for its errors. An Indian SBAS called GAGAN (GPS Aided Geo Augmented Navigation), developed for the Airports Authority of India (AAI) by Indian Space Research Organization (ISRO) is currently being installed and proven for aviation and other use. The uncertain propagation delay of signals through the ionosphere is the most important contributor of error in GPS positioning, its maximal elimination is a major task of SBAS overlays. Ionospheric delays have steady, cyclic, and irregular components. The last types are of particular concern because they are unpredictable. This thesis deals with ionospheric depletion, an important phenomenon of this class that is specific to tropical regions like India and hence have not been well studied in the context of other SBAS systems of the world which cover mid-latitude domains. Depletion is an ionospheric phenomenon in which the density of electrons dips suddenly and then returns close to the previous value. It poses a challenge to the model adopted for ionospheric delay estimation since it may not be detectable by ground systems be- cause of its localized nature, and its occurrence and intensity cannot be predicted. In this work we have analyzed the depletion characteristics over the Indian region such as its distribution, frequency of occurrence, and depth and duration parameters. We have then studied and implemented an existing algorithm to detect a depletion from the Total Electron Content (TEC) data. This algorithm has been found to be inaccurate for estimation of depletion duration, and we have proposed an improved algorithm for depletion detection and shown it to be more suitable for the Indian SBAS, GAGAN. The algorithm utilizes multiple thresholds for depletion detection in order to improve performance in the presence of irregularities including noise. These thresholds are determined by analyzing real TEC data containing depletion events over the Indian region. The detected depletion events are those that have a strong likelihood of contributing large range errors and degrading GAGAN's reliability. The thresholds include depletion parameters such as the depth, duration, rate of change of TEC, and the rate of change of slope of the TEC curve. The characterization of depletion events over the Indian region yielded useful insights into the behaviour of the phenomenon. It was observed that the depletion events were invariably present post-sunset, between 1900 and 0200 hrs. This observation is consistent with the other studies on plasma bubbles so far. The average depth of the depletion was found to be about 3.31 meters of propagation delay while the strongest depletion corresponds to about 5.04 meters of delay. The latter observation impresses upon the need to detect and study the phenomenon of depletion since it is capable of causing a significant loss of accuracy and reliability to the system. The duration of the depletion was found to range from about 10 min to 2.35 hours. In addition, a statistical study of the relationship among the different parameters and a study devoted to now-casting of depletion was made to get a more quantitative insight into the phenomenon of depletion. Scintillation is another phenomenon occurring in the ionosphere which causes rapid fluctuations of phase and amplitude of the signal due to TEC variations in the ionosphere. The occurrences of depletion were observed to be accompanied by scintillation, as also noted in previous studies. The correlation of depletion and scintillation was studied using the data available for this research. A spatial characterization of the depletion events was also investigated using the same temporal TEC data from neighbouring stations which were relatively close to each other. This study addressed the movement of the plasma bubble with respect to the advection speed and direction with definite results. Attention was also devoted to the spatial dimension of the bubble as observed from various stations. Contributions to this variability in the apparent spatial extent comes from the observation of the depletion event from varying lines-of-sight corresponding to different GPS satellites which are also moving, and the differential `slicing' effect because of the location of the stations with respect to the plasma bubble, in addition to the evolution of the bubble during transit. The detection of depletion and its temporal characterization, in addition to the knowledge of its spatial extent and motion, can provide very useful insights on the behaviour of a depletion event and over the ionosphere in general. This knowledge and the mechanism for detection can help to improve the quality and dependability of the information provided by SBAS systems, in particular the Indian GAGAN system, for improved navigation in this part of the world. The present thesis aims to make a significant contribution in this direction.