Ad majorem dei gloriam- Espace de dieu et domaine des hommes, analyse des missions jesuites du paracuaria (1610 – 1767) a partir de l’archeologie phenomenologique, cas d’étude Nuestra Señora de Loreto (i et ii) et San Ignacio Mini (i et ii)

Méthodologie: Modèle interprétatif de l’archéologie phénoménologique.

Jean Pierron (1631-1700) : missionnaire, diplomate et peintre en Amérique.

La présente recherche se propose de retracer la vie et l’œuvre du père jésuite Jean Pierron (1631-1701), qui, venu de Lorraine, a contribué à la réouverture des missions iroquoises en Nouvelle-France. Arrivé dans la colonie en juin 1667, Pierron, se fit introduire auprès des populations autochtones par Jean Talon, après quoi il eut en charge un territoire d'environ une demi-douzaine de villages agniers de la vallée de l'Hudson. Après avoir livré ses premières impressions, le jésuite mit au point son programme apostolique, faisant appel à une méthode « audio-visuelle » fondée sur le dessin didactique. Mais le jésuite fut aussi un formidable voyageur, qui se rendit non seulement en Iroquoisie, mais aussi en Nouvelle-Angleterre. Il semble bien que ce soit grâce à de précieux réseaux de connaissances en dehors de ceux de la Compagnie de Jésus qu'il put entreprendre un tel voyage. La biographie de ce missionnaire-polyglotte, diplomate et peintre, souligne entre autre choses, l’importance du contexte stratégique et politique plus vaste des missions françaises en Amérique au XVIIe siècle.

Missions du Canada, lettres de Jésuites, etc. (XVIIe-XVIIIe siècles).

Contient : Relation des affaires des Iroquois (1692-1693) ; « Lettre du R. P. Dablon », sur la mort du P. Chaumont, missionnaire au Canada (28 févr. 1693) ; « Lettre du P. Jacques Gravier, en forme de Journal de la mission de l'Immaculée-Conception de N.-D. aux Illinois, ce 15 févr 1694 » ; « Parolles dites par Tegamsorens à Mgr. le comte de Frontenac, au nom des cinq nations Iroquoises,... a Québec, le 23 may 1694 » ; Lettres de la mission de Saint-François de Sales (1694) ; Lettres de différents PP. Jésuites ; plusieurs de ces lettres sont adressées aux PP. Le Gobien et de Vitry, à Nantes, et de Lynières, à la Flèche (1693-1694) ; Lettre relative au collège d'Auxerre (1762) ; « Bureau universel d'adresses et de renseignemens pour les mariages, les établissemens de commerce... » (XIXe siècle) ; « Lettre à un docteur en théologie par un de ses amis, au sujet de l'emprisonnement de M. Blache »

Mémoire historique sur la décadence et la ruine des missions des Jésuites dans la bassin de la Plata, leur état actuel /

On spine: Mémoire des missions des Jésuites.

Sensors for missions

An onboard payload may be seen in most instances as the “Raison d’Etre” for a UAV. It will define its capabilities, usability and hence market value. Large and medium UAV payloads exhibit significant differences in size and computing capability when compared with small UAVs. The latter have stringent size, weight, and power requirements, typically referred as SWaP, while the former still exhibit endless appetite for compute capability. The tendency for this type of UAVs (Global Hawk, Hunter, Fire Scout, etc.) is to increase payload density and hence processing capability. An example of this approach is the Northrop Grumman MQ-8 Fire Scout helicopter, which has a modular payload architecture that incorporates off-the-shelf components. Regardless of the UAV size and capabilities, advances in miniaturization of electronics are enabling the replacement of multiprocessing, power-hungry general-purpose processors for more integrated and compact electronics (e.g., FPGAs). Payloads play a significant role in the quality of ISR (intelligent, surveillance, and reconnaissance) data, and also in how quick that information can be delivered to the end user. At a high level, payloads are important enablers of greater mission autonomy, which is the ultimate aim in every UAV. This section describes common payload sensors and introduces two examples cases in which onboard payloads were used to solve real-world problems. A collision avoidance payload based on electro optical (EO) sensors is first introduced, followed by a remote sensing application for power line inspection and vegetation management.

Towards coordinated multirobot missions for lunar sample collection in an unknown environment

In this paper, the recent results of the space project IMPERA are presented. The goal of IMPERA is the development of a multirobot planning and plan execution architecture with a focus on a lunar sample collection scenario in an unknown environment. We describe the implementation and verification of different modules that are integrated into a distributed system architecture. The modules include a mission planning approach for a multirobot system and modules for task and skill execution within a lunar use-case scenario. The skills needed for the test scenario include cooperative exploration and mapping strategies for an unknown environment, the localization and classification of sample containers using a novel approach of semantic perception, and the skill of transporting sample containers to a collection point using a mobile manipulation robot. Additionally, we present our approach of a reliable communication framework that can deal with communication loss during the mission. Several modules are tested within several experiments in the domain of planning and plan execution, communication, coordinated exploration, perception, and object transportation. An overall system integration is tested on a mission scenario experiment using three robots.

Search Strategies for Multiple UAV Search and Destroy Missions

Multiple UAVs are deployed to carry out a search and destroy mission in a bounded region. The UAVs have limited sensor range and can carry limited resources which reduce with use. The UAVs perform a search task to detect targets. When a target is detected which requires different type and quantities of resources to completely destroy, then a team of UAVs called as a coalition is formed to attack the target. The coalition members have to modify their route to attack the target, in the process, the search task is affected, as search and destroy tasks are coupled. The performance of the mission is a function of the search and the task allocation strategies. Therefore, for a given task allocation strategy, we need to devise search strategies that are efficient. In this paper, we propose three different search strategies namely; random search strategy, lanes based search strategy and grid based search strategy and analyze their performance through Monte-Carlo simulations. The results show that the grid based search strategy performs the best but with high information overhead.

UAV Grouping and Coordination Tactics for Ground Attack Missions

Grouping and coordination tactics for ground attack missions by a heterogeneous mix of reconnaissance, enemy suppression, and attack unmanned aerial vehicles (UAVs) is presented. Dubins' paths are used to determine the optimal number of attack UAVs and their positional and heading freedoms, as functions of weapon seeker range and field of view. A generic battlefield scenario with layered defense is created and the tactics are evaluated on a Group Flyer simulation platform for both nominal and off-nominal conditions.

Advancing EDL technologies for future space missions : from ground testing facilities to ablative heatshields

Motivated by recent MSL results where the ablation rate of the PICA heatshield was over-predicted, and staying true to the objectives outlined in the NASA Space Technology Roadmaps and Priorities report, this work focuses on advancing EDL technologies for future space missions.

Due to the difficulties in performing flight tests in the hypervelocity regime, a new ground testing facility called the vertical expansion tunnel is proposed. The adverse effects from secondary diaphragm rupture in an expansion tunnel may be reduced or eliminated by orienting the tunnel vertically, matching the test gas pressure and the accelerator gas pressure, and initially separating the test gas from the accelerator gas by density stratification. If some sacrifice of the reservoir conditions can be made, the VET can be utilized in hypervelocity ground testing, without the problems associated with secondary diaphragm rupture.

The performance of different constraints for the Rate-Controlled Constrained-Equilibrium (RCCE) method is investigated in the context of modeling reacting flows characteristic to ground testing facilities, and re-entry conditions. The effectiveness of different constraints are isolated, and new constraints previously unmentioned in the literature are introduced. Three main benefits from the RCCE method were determined: 1) the reduction in number of equations that need to be solved to model a reacting flow; 2) the reduction in stiffness of the system of equations needed to be solved; and 3) the ability to tabulate chemical properties as a function of a constraint once, prior to running a simulation, along with the ability to use the same table for multiple simulations.

Finally, published physical properties of PICA are compiled, and the composition of the pyrolysis gases that form at high temperatures internal to a heatshield is investigated. A necessary link between the composition of the solid resin, and the composition of the pyrolysis gases created is provided. This link, combined with a detailed investigation into a reacting pyrolysis gas mixture, allows a much needed consistent, and thorough description of many of the physical phenomena occurring in a PICA heatshield, and their implications, to be presented.

Through the use of computational fluid mechanics and computational chemistry methods, significant contributions have been made to advancing ground testing facilities, computational methods for reacting flows, and ablation modeling.

Multi-objective optimization for multiphase orbital rendezvous missions

A multi-objective optimization approach was proposed for multiphase orbital rendezvous missions and validated by application to a representative numerical problem. By comparing the Pareto fronts obtained using the proposed method, the relationships between the three objectives considered are revealed, and the influences of other mission parameters, such as the sensors' field of view, can also be analyzed effectively. For multiphase orbital rendezvous missions, the tradeoff relationships between the total velocity increment and the trajectory robustness index as well as between the total velocity increment and the time of flight are obvious and clear. However, the tradeoff relationship between the time of flight and the trajectory robustness index is weak, especially for the four- and five-phase missions examined. The proposed approach could be used to reorganize a stable rendezvous profile for an engineering rendezvous mission, when there is a failure that prevents the completion of the nominal mission.

Davis, soldier missionary : a biography of Rev. Jerome D. Davis, D.D., Lieut-Colonel of volunteers and for thirty-nine years a missionary of the American Board of Commissioners for Foreign Missions in Japan

http://www.archive.org/details/davissoldiermiss00davirich

Educational missions.

http://www.archive.org/details/educationalmissi008437mbp

Memorial volume of the first fifty years of the American board of commissioners for foreign missions.

http://www.archive.org/details/memorialvolumeof00andeuoft

Christian missions ; their agents, and their results / by T.W.M. Marshall.

http://www.archive.org/details/a592254601marsuoft

Poor Lo! Early Indian missions. A memorial. By Walter N. Wyeth.

http://www.archive.org/details/poorloearlyindia00wyetiala