Aircraft trajectory simulator using a three degrees of freedom aircraft point mass model

Aircraft Operators Companies (AOCs) are always willing to keep the cost of a flight as low as possible. These costs could be modelled using a function of the fuel consumption, time of flight and fixed cost (over flight cost, maintenance, etc.). These are strongly dependant on the atmospheric conditions, the presence of winds and the aircraft performance. For this reason, much research effort is being put in the development of numerical and graphical techniques for defining the optimal trajectory. This paper presents a different approach to accommodate AOCs preferences, adding value to their activities, through the development of a tool, called aircraft trajectory simulator. This tool is able to simulate the actual flight of an aircraft with the constraints imposed. The simulator is based on a point mass model of the aircraft. The aim of this paper is to evaluate 3DoF aircraft model errors with BADA data through real data from Flight Data Recorder FDR. Therefore, to validate the proposed simulation tool a comparative analysis of the state variables vector is made between an actual flight and the same flight using the simulator. Finally, an example of a cruise phase is presented, where a conventional levelled flight is compared with a continuous climb flight. The comparison results show the potential benefits of following user-preferred routes for commercial flights.

Comment on "From geodesics of the multipole solutions to the perturbed Kepler problem"

In this Comment we explain the discrepancies mentioned by the authors between their results and ours about the in?uence of the gravitational quadrupole moment in the perturbative calculation of corrections to the precession of the periastron of quasielliptical Keplerian equatorial orbits around a point mass. The discrepancy appears to be a consequence of two different calculations of the angular momentum of the orbits.

O Botafumeiro: parametric pumping in the Middle Age

The pendular motion of a giant censer (O Botafumeiro) that hangs in the transept of the cathedral of Santiago de Compostela, and is cyclically pumped by men who pull at the supporting rope, is analyzed. Maximum angular amplitude attainable, and number of cycles and time needed to attain it, are calculated; the results agree with observed values (~ 82°, ~ 17 cycles, ~ 80 seconds) to the few percent accuracy of both the analysis and the observations and parameter measurements. The energy gain in a pumping cycle is obtained for an arbitrary pumping procedure to two orders in the small fractional change of pendular length; the relevance of the ratio (characteristic radial acceleration during pumping)/g to the gain is discussed- Effects due to rope mass, air drag on both Censer and rope, and the fact that the Censer is not a point mass, are considered. If the pumping cycle is inverted once the maximum amplitude has been attained, the Censer could be swiftly brought to rest, avoiding the usual violent stop. Historically recorded accidents, rope shape, and the influence of relevant parameters on the motion are discussed.

Analysis of the geometric altimetry to support aircraft optimal trajectories within the future 4d trajectory management

Over the past few years, the common practice within air traffic management has been that commercial aircraft fly by following a set of predefined routes to reach their destination. Currently, aircraft operators are requesting more flexibility to fly according to their prefer- ences, in order to achieve their business objectives. Due to this reason, much research effort is being invested in developing different techniques which evaluate aircraft optimal trajectory and traffic synchronisation. Also, the inefficient use of the airspace using barometric altitude overall in the landing and takeoff phases or in Continuous Descent Approach (CDA) trajectories where currently it is necessary introduce the necessary reference setting (QNH or QFE). To solve this problem and to permit a better airspace management born the interest of this research. Where the main goals will be to evaluate the impact, weakness and strength of the use of geometrical altitude instead of the use of barometric altitude. Moreover, this dissertation propose the design a simplified trajectory simulator which is able to predict aircraft trajectories. The model is based on a three degrees of freedom aircraft point mass model that can adapt aircraft performance data from Base of Aircraft Data, and meteorological information. A feature of this trajectory simulator is to support the improvement of the strategic and pre-tactical trajectory planning in the future Air Traffic Management. To this end, the error of the tool (aircraft Trajectory Simulator) is measured by comparing its performance variables with actual flown trajectories obtained from Flight Data Recorder information. The trajectory simulator is validated by analysing the performance of different type of aircraft and considering different routes. A fuel consumption estimation error was identified and a correction is proposed for each type of aircraft model. In the future Air Traffic Management (ATM) system, the trajectory becomes the fundamental element of a new set of operating procedures collectively referred to as Trajectory-Based Operations (TBO). Thus, governmental institutions, academia, and industry have shown a renewed interest for the application of trajectory optimisation techniques in com- mercial aviation. The trajectory optimisation problem can be solved using optimal control methods. In this research we present and discuss the existing methods for solving optimal control problems focusing on direct collocation, which has received recent attention by the scientific community. In particular, two families of collocation methods are analysed, i.e., Hermite-Legendre-Gauss-Lobatto collocation and the pseudospectral collocation. They are first compared based on a benchmark case study: the minimum fuel trajectory problem with fixed arrival time. For the sake of scalability to more realistic problems, the different meth- ods are also tested based on a real Airbus 319 El Cairo-Madrid flight. Results show that pseudospectral collocation, which has shown to be numerically more accurate and computa- tionally much faster, is suitable for the type of problems arising in trajectory optimisation with application to ATM. Fast and accurate optimal trajectory can contribute properly to achieve the new challenges of the future ATM. As atmosphere uncertainties are one of the most important issues in the trajectory plan- ning, the final objective of this dissertation is to have a magnitude order of how different is the fuel consumption under different atmosphere condition. Is important to note that in the strategic phase planning the optimal trajectories are determined by meteorological predictions which differ from the moment of the flight. The optimal trajectories have shown savings of at least 500 [kg] in the majority of the atmosphere condition (different pressure, and temperature at Mean Sea Level, and different lapse rate temperature) with respect to the conventional procedure simulated at the same atmosphere condition.This results show that the implementation of optimal profiles are beneficial under the current Air traffic Management (ATM).

A General Purpose Configurable Controller for Indoors and Outdoors GPS-Denied Navigation for Multirotor Unmanned Aerial Vehicles

This research on odometry based GPS-denied navigation on multirotor Unmanned Aerial Vehicles is focused among the interactions between the odometry sensors and the navigation controller. More precisely, we present a controller architecture that allows to specify a speed specified flight envelope where the quality of the odometry measurements is guaranteed. The controller utilizes a simple point mass kinematic model, described by a set of configurable parameters, to generate a complying speed plan. For experimental testing, we have used down-facing camera optical-flow as odometry measurement. This work is a continuation of prior research to outdoors environments using an AR Drone 2.0 vehicle, as it provides reliable optical flow on a wide range of flying conditions and floor textures. Our experiments show that the architecture is realiable for outdoors flight on altitudes lower than 9 m. A prior version of our code was utilized to compete in the International Micro Air Vehicle Conference and Flight Competition IMAV 2012. The code will be released as an open-source ROS stack hosted on GitHub.

Caracterización de las Propiedades Dinámicas de la Seda de Araña

El término Biomimética se ha hecho común en los medios científicos, se refiere al trabajo de diversos científicos (ingenieros, químicos, físicos, biólogos, etc.) que tratan de copiar los procesos biológicos y aplicarlos en distintas áreas tecnológicas y científicas. En este campo científico, uno de los productos naturales que llama más la atención es la telaraña. Numerosos científicos en todo el mundo tratan de copiar las propiedades de la seda que produce la araña, y lo más interesante es que hasta intentan reproducir el método que usan las arañas para fabricar la seda De la bibliografía consultada, se desprende la importancia de la seda en la vida de las arañas, pues toda actividad que realizan tiene que ver de alguna manera con este elemento. Uno de estos elementos es la tela de araña orbicular, que representa el objeto principal para la supervivencia de la araña y su especie. Las investigaciones realizadas en esta línea nos proporcionan información sobre sus magníficas propiedades mecánicas como de resistencia, elasticidad y tenacidad del hilo de seguridad (seda MA) segregada por una araña de la especie Argiope Argentata. El enfoque de la presente tesis se realiza desde una perspectiva analítica-experimental, tomando a la tela de araña como una clase especial de sistemas pretensados, llamados Tensegrity Structures. Se desarrolla un modelo conceptual que describe en forma aproximada el comportamiento dinámico de una estructura hecha de seda MA. Haciendo uso de las técnicas experimentales de vibraciones libres se realizan los ensayos experimentales. La evaluación de los resultados analíticos y experimentales reflejan claramente que la función principal de la tela de araña es la de convertir energía cinética en energía de deformación y primordialmente en energía de disipación, el cual se efectúa gracias a las propiedades viscoelásticas de la seda. La araña en forma instintiva recurre a la ayuda del aire (como elemento disipador) para el buen funcionamiento de la tela de araña al momento de la captura de las presas, disipándose el 99% de la energía total en los tres primeros ciclos de oscilación de la tela de araña luego del impacto de la presa. ABSTRACT The term Biomimetic has become a very common word in the scientific world to describe the reproduction of the biological processes and its application in the different technogycal and scientific areas. One of the most notably natural product of this field is the Spiderweb. In the present days, many scientists of the world are active working in the reproduction of the proprieties of the Spiderweb. Most interesting even more, is the attempt to reproduce the process of the production of the Spiderweb by the spider. Most of the bibliography references deals whit the importance of the Spiderweb silk in the life of the spiders and the orbicular Spiderweb represents the spider survival and of the species. The research conducted in this field provide information about the excellent mechanical proprieties such us strength, elasticity and tenacity of the safety fiber (silk MA Drag-line) segregated by a spider of the Argiope Argentata species. The present work is oriented to an analytical and experimental study considering the Spiderweb as a special class of pre-stressed systems called Tensegrity (tensional integrity) structures. A conceptual model maked up by a cord und a point mass has been developed. This model approximates the dynamics performance of the structure made of the silk MA. The evaluation of the analytical and experimental results clear described that the main function of the Spiderweb is the transformation of the kinetic energy in deformation energy, and mainly in dissipation energy thank to the viscoelastic proprieties of the Spiderweb. With the help of the Spiderweb, the spider instinctively resorts to the help of the surroundings air as a dissipation element. This permits to dissipative the 99% of the total energy during the three first oscillations cycles of the web after the impact of the victim.

A low-mass impact sensor for high-speed firmness sensing of fruits.

A low-mass impact sensor for high-speed firmness sensing of fruits was built and tested. Results of tests with a rubber ball indicated that the impact measurement was not sensitive to the distance between the impactor and the impacting surface of the sample within the range of 8 to 23 mm, and was not sensitive to how the sample was held. Tests with kiwifruits and peaches show good correlation between firmness readings obtained with the impact sensor and those obtained with the penetrometer. The best correlation was between the slope of the impact curve (at mid-point) and the force-deformation firmness. Preliminary test showed that the sensor could sense fruit firmness at a speed of 5 fruits/s.

Reduction of critical mass in a chemotaxis system by external application of a chemoattractant

In this paper we study non-negative radially symmetric solutions of a parabolic-elliptic Keller-Segel system. The system describes the chemotactic movement of cells under the additional circumstance that an external application of a chemo attractant at a distinguished point is introduced.