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Wettbewerbsregeln (§§ 24-27)
(2022)
Following the recent successful landings and occasional re-awakenings of PHILAE, the lander carried aboard ROSETTA to comet 67P/Churyumov-Gerasimenko, and the launch of the Mobile Asteroid Surface Scout, MASCOT, aboard the HAYABUSA2 space probe to asteroid (162173) Ryugu we present an overview of the characteristics and peculiarities of small spacecraft missions to small solar system bodies (SSSB). Their main purpose is planetary science which is transitioning from a ‘pure’ science of observation of the distant to one also supporting in-situ applications relevant for life on Earth. Here we focus on missions at the interface of SSSB science and planetary defence applications. We provide a brief overview of small spacecraft SSSB missions and on this background present recent missions, projects and related studies at the German Aerospace Center, DLR, that contribute to the worldwide planetary defence community. These range from Earth orbit technology demonstrators to active science missions in interplanetary space. We provide a summary of experience from recently flown missions with DLR participation as well as a number of studies. These include PHILAE, the lander of ESA’s ROSETTA comet rendezvous mission now on the surface of comet 67P/Churyumov-Gerasimenko, and the Mobile Asteroid Surface Scout, MASCOT, now in cruise to the ~1 km diameter C-type near-Earth asteroid (162173) Ryugu aboard the Japanese sample-return probe HAYABUSA2. We introduce the differences between the conventional methods employed in the design, integration and testing of large spacecraft and the new approaches developed by small spacecraft projects. We expect that the practical experience that can be gained from projects on extremely compressed timelines or with high-intensity operation phases on a newly explored small solar system body can contribute significantly to the study, preparation and realization of future planetary defence related missions. One is AIDA (Asteroid Impact & Deflection Assessment), a joint effort of ESA, JHU/APL, NASA, OCA and DLR, combining JHU/APL’s DART (Double Asteroid Redirection Test) and ESA’s AIM (Asteroid Impact Monitor) spacecraft in a mission towards near-Earth binary asteroid system (65803) Didymos. DLR is currently applying MASCOT heritage and lessons learned to the design of MASCOT2, a lander for the AIM mission to support a bistatic low frequency radar experiment with PHILAE/ROSETTA CONSERT heritage to explore the inner structure of Didymoon which is the designated impact target for DART.
We present the novel concept of a combined drilling and melting probe for subsurface ice research. This probe, named “IceMole”, is currently developed, built, and tested at the FH Aachen University of Applied Sciences’ Astronautical Laboratory. Here, we describe its first prototype design and report the results of its field tests on the Swiss Morteratsch glacier. Although the IceMole design is currently adapted to terrestrial glaciers and ice shields, it may later be modified for the subsurface in-situ investigation of extraterrestrial ice, e.g., on Mars, Europa, and Enceladus. If life exists on those bodies, it may be present in the ice (as life can also be found in the deep ice of Earth).
Interplanetary trajectories for low-thrust spacecraft are often characterized by multiple revolutions around the sun. Unfortunately, the convergence of traditional trajectory optimizers that are based on numerical optimal control methods depends strongly on an adequate initial guess for the control function (if a direct method is used) or for the starting values of the adjoint vector (if an indirect method is used). Especially when many revolutions around the sun are re-
quired, trajectory optimization becomes a very difficult and time-consuming task that involves a lot of experience and expert knowledge in astrodynamics and optimal control theory, because an adequate initial guess is extremely hard to find. Evolutionary neurocontrol (ENC) was proposed as a smart method for low-thrust trajectory optimization that fuses artificial neural networks and evolutionary algorithms to so-called evolutionary neurocontrollers (ENCs) [1]. Inspired by natural archetypes, ENC attacks the trajectoryoptimization problem from the perspective of artificial intelligence and machine learning, a perspective that is quite different from that of optimal control theory. Within the context of ENC, a trajectory is regarded as the result of a spacecraft steering strategy that maps permanently the actual spacecraft state and the actual target state onto the actual spacecraft control vector. This way, the problem of searching the optimal spacecraft trajectory is equivalent to the problem of searching (or "learning") the optimal spacecraft steering strategy. An artificial neural network is used to implement such a spacecraft steering strategy. It can be regarded as a parameterized function (the network function) that is defined by the internal network parameters. Therefore, each distinct set of network parameters defines a different network function and thus a different steering strategy. The problem of searching the optimal steering strategy is now equivalent to the problem of searching the optimal set of network parameters. Evolutionary algorithms that work on a population of (artificial) chromosomes are used to find the optimal network parameters, because the parameters can be easily mapped onto a chromosome. The trajectory optimization problem is solved when the optimal chromosome is found. A comparison of solar sail trajectories that have been published by others [2, 3, 4, 5] with ENC-trajectories has shown that ENCs can be successfully applied for near-globally optimal spacecraft control [1, 6] and that they are able to find trajectories that are closer to the (unknown) global optimum, because they explore the trajectory search space more exhaustively than a human expert can do. The obtained trajectories are fairly accurate with respect to the terminal constraint. If a more accurate trajectory is required, the ENC-solution can be used as an initial guess for a local trajectory optimization method. Using ENC, low-thrust trajectories can be optimized without an initial guess and without expert attendance.
Here, new results for nuclear electric spacecraft and for solar sail spacecraft are presented and it will be shown that ENCs find very good trajectories even for very difficult problems. Trajectory optimization results are presented for 1. NASA's Solar Polar Imager Mission, a mission to attain a highly inclined close solar orbit with a solar sail [7] 2. a mission to de ect asteroid Apophis with a solar sail from a retrograde orbit with a very-high velocity impact [8, 9] 3. JPL's \2nd Global Trajectory Optimization Competition", a grand tour to visit four asteroids from different classes with a NEP spacecraft
his report summarizes the results of a workshop on Groupware related task design which took place at the International Conference on Supporting Group Work Group'99, Arizona, from 14 th to 17 th November 1999.
The workshop was addressed to people from different
viewpoints, backgrounds, and domains:
- Researchers dealing with questions of task analysis
and task modeling for Groupware application from an
academic point of view. They may contribute modelbased design
approaches or theoretically oriented
work
- Practitioners with experience in the design and
everyday use of groupware systems. They might refer
to the practical side of the topic: "real" tasks, "real"
problems, "real" users, etc.
Digital start-ups are perceived as an engine for innovation and job promotor. While success factors for non-IT start-ups have already been extensively researched, this study sheds light on digital entrepreneurs, whose business model relies primarily on services based on digital technologies. Applying the Grounded Theory method, we identify relevant environmental success factors for digital entrepreneurs. The study’s research contribution is threefold. First, we provide 16 relevant and less relevant environmental success factors, which enables a comparison with prior identified factors. We found out that several prior environmental success factors, such as accessibility to transportation or the availability of land and facilities are less relevant for a digital entrepreneur. Second, we derive and discuss hypotheses for the influence of these factors on digital start-up success. Third, we present a theoretical model that lays the foundation for explaining the environmental influence on digital
entrepreneurship success.
A laser-enhanced solar sail is a solar sail that is not solely propelled by solar radiation but additionally by a laser beam that illuminates the sail. This way, the propulsive acceleration of the sail results from the combined action of the solar and the laser radiation pressure onto the sail. The potential source of the laser beam is a laser satellite that coverts solar power (in the inner solar system) or nuclear power (in the outer solar system) into laser power. Such a laser satellite (or many of them) can orbit anywhere in the solar system and its optimal orbit (or their optimal orbits) for a given mission is a subject for future research. This contribution provides the model for an ideal laser-enhanced solar sail and investigates how a laser can enhance the thrusting capability of such a sail. The term ”ideal” means that the solar sail is assumed to be perfectly reflecting and that the laser beam is assumed to have a constant areal power density over the whole sail area. Since a laser beam has a limited divergence, it can provide radiation pressure at much larger solar distances and increase the radiation pressure force into the desired direction. Therefore, laser-enhanced solar sails may make missions feasible, that would otherwise have prohibitively long flight times, e.g. rendezvous missions in the outer solar system. This contribution will also analyze exemplary mission scenarios and present optimial trajectories without laying too much emphasis on the design and operations of the laser satellites. If the mission studies conclude that laser-enhanced solar sails would have advantages with respect to ”traditional” solar sails, a detailed study of the laser satellites and the whole system architecture would be the second next step
Physical interaction with small solar system bodies (SSSB) is key for in-situ resource utilization (ISRU). The design of mining missions requires good understanding of SSSB properties, including composition, surface and interior structure, and thermal environment. But as the saying goes "If you've seen one asteroid, you've seen one Asteroid": Although some patterns may begin to appear, a stable and reliable scheme of SSSB classification still has to be evolved. Identified commonalities would enable generic ISRU technology and spacecraft design approaches with a high degree of re-use. Strategic approaches require much broader in-depth characterization of the SSSB populations of interest to the ISRU community. The DLR-ESTEC GOSSAMER Roadmap Science Working Groups identified target-flexible Multiple Near-Earth asteroid (NEA) Rendezvous (MNR) as one of the missions only feasible with solar sail propulsion, showed the ability to access any inclination and a wide range of heliocentric distances as well as continuous operation close to Earth's orbit where low delta-v objects reside.
The search for life on Mars and in the Solar System - strategies, logistics and infrastructures
(2018)
The question "Are we alone in the Universe?" is perhaps the most fundamental one that affects mankind. How can we address the search for life in our Solar System? Mars, Enceladus and Europa are the focus of the search for life outside the terrestrial biosphere. While it is more likely to find remnants of life (fossils of extinct life) on Mars because of its past short time window of the surface habitability, it is probably more likely to find traces of extant life on the icy moons and ocean worlds of Jupiter and Saturn. Nevertheless, even on Mars there could still be a chance to find extant life in niches near to the surface or in just discovered subglacial lakes beneath the South Pole ice cap. Here, the different approaches for the detection of traces of life in the form of biosignatures including pre-biotic molecules will be presented. We will outline the required infrastructure for this enterprise and give examples of future mission concepts to investigate the presence of life on other planets and moons. Finally, we will provide suggestions on methods, techniques, operations and strategies for preparation and realization of future life detection missions.
For now, the Planetary Defense Conference Exercise 2021's incoming fictitious(!), asteroid, 2021 PDC, seems headed for impact on October 20th, 2021, exactly 6 months after its discovery. Today (April 26th, 2021), the impact probability is 5%, in a steep rise from 1 in 2500 upon discovery six days ago. We all know how these things end. Or do we? Unless somebody kicked off another headline-grabbing media scare or wants to keep civil defense very idle very soon, chances are that it will hit (note: this is an exercise!). Taking stock, it is barely 6 months to impact, a steadily rising likelihood that it will actually happen, and a huge uncertainty of possible impact energies: First estimates range from 1.2 MtTNT to 13 GtTNT, and this is not even the worst-worst case: a 700 m diameter massive NiFe asteroid (covered by a thin veneer of Ryugu-black rubble to match size and brightness), would come in at 70 GtTNT. In down to Earth terms, this could be all between smashing fireworks over some remote area of the globe and a 7.5 km crater downtown somewhere. Considering the deliberate and sedate ways of development of interplanetary missions it seems we can only stand and stare until we know well enough where to tell people to pack up all that can be moved at all and save themselves. But then, it could just as well be a smaller bright rock. The best estimate is 120 m diameter from optical observation alone, by 13% standard albedo. NASA's upcoming DART mission to binary asteroid (65803) Didymos is designed to hit such a small target, its moonlet Dimorphos. The Deep Impact mission's impactor in 2005 successfully guided itself to the brightest spot on comet 9P/Tempel 1, a relatively small feature on the 6 km nucleus. And 'space' has changed: By the end of this decade, one satellite communication network plans to have launched over 11000 satellites at a pace of 60 per launch every other week. This level of series production is comparable in numbers to the most prolific commercial airliners. Launch vehicle production has not simply increased correspondingly – they can be reused, although in a trade for performance. Optical and radio astronomy as well as planetary radar have made great strides in the past decade, and so has the design and production capability for everyday 'high-tech' products. 60 years ago, spaceflight was invented from scratch within two years, and there are recent examples of fast-paced space projects as well as a drive towards 'responsive space'. It seems it is not quite yet time to abandon all hope. We present what could be done and what is too close to call once thinking is shoved out of the box by a clear and present danger, to show where a little more preparedness or routine would come in handy – or become decisive. And if we fail, let's stand and stare safely and well instrumented anywhere on Earth together in the greatest adventure of science.
Low-thrust space propulsion systems enable flexible high-energy deep space missions, but the design and optimization of the interplanetary transfer trajectory is usually difficult. It involves much experience and expert knowledge because the convergence behavior of traditional local trajectory optimization methods depends strongly on an adequate initial guess. Within this extended abstract, evolutionary neurocontrol, a method that fuses artificial neural networks and evolutionary algorithms, is proposed as a smart global method for low-thrust trajectory optimization. It does not require an initial guess. The implementation of evolutionary neurocontrol is detailed and its performance is shown for an exemplary mission.
Innovative interplanetary deep space missions, like a main belt asteroid sample
return mission, require ever larger velocity increments (∆V s) and thus ever
more demanding propulsion capabilities. Providing much larger exhaust velocities than chemical high-thrust systems, electric low-thrust space-propulsion
systems can significantly enhance or even enable such high-energy missions. In
1995, a European-Russian Joint Study Group (JSG) presented a study report
on “Advanced Interplanetary Missions Using Nuclear-Electric Propulsion”
(NEP). One of the investigated reference missions was a sample return (SR)
from the main belt asteroid (19) Fortuna. The envisaged nuclear power plant,
Topaz-25, however, could not be realized and also the worldwide developments
in space reactor hardware stalled. In this paper, we investigate, whether such
a mission is also feasible using a solar electric propulsion (SEP) system and
compare our SEP results to corresponding NEP results.
Sen(se)sation : VR Produktvision mit multisensorischem Einfluss
auf die menschliche Wahrnehmung
(2022)
Das Sen(se)sation VR-Produktkonzept ermöglicht Nutzer*Innen die nahezu vollkommen realistische Darstellung virtuell generierter Welten. Das Konzept ist in genauer Betrachtung des aktuellen Technikstands und der Analyse von Zukunftstrends konzipiert worden und stellt eine Produktvision dar, die in spätestens 5 Jahren problemlos umsetzbar sein wird. Um nicht den Eindruck einer unfundierten Zukunftsvision zu erzeugen, wurde sich bei der Konstruktion der integrierten Features auf aktuell erhältliche Vergleichsprodukte bezogen. Das Sen(se)sation VR System zeigt neue Möglichkeiten die Gestaltungs- und Technikbereich derzeitiger VR Brillen und Controller. Durch die Fokussierung des Produkts auf die Manipulation und Stimulation der fünf Hauptsinne des Menschen wird ein so hoher Grad der Immersion erzeugt, dass die Wahrnehmung von Realität und Virtualität beinah verschwimmen könnte.
Es ist nachweislich gesünder und häufig günstiger selber zu kochen und es gibt dem Menschen mehr Kontrolle über seine Ernährung.
Bis dato wird keine Küchenmaschine angeboten, die von blinden Menschen bedient werden kann, obwohl gerade solche Produkte den Alltag dieser Gruppe enorm vereinfachen könnten. „Clu.“ ist ein modulares Küchensystem, welches von einer App unterstützt wird. Die Basis besteht aus einer Küchenmaschine, die über Sprache und haptische Bedienelemente gesteuert wird. Durch die Anwendung des Mehr-Sinne-Prinzip, der Simplifizierung von Funktionen und der Einbindung von Smart Home Komponenten werden nicht nur Menschen mit Sehbeeinträchtigungen profitieren. Beispielsweise funktioniert das Kochen nach Rezept nun ähnlich wie das Hören eines Hörbuches und die User können sich dem in ihrem favorisierten Tempo annehmen. „Clu.“ ist ein Ansatz für eine neue Kategorie von Produkten, die zeigen, wie attraktiv inklusivere Produktlösungen aussehen können.
bulk : Konzeption und Gestaltung einer mobilen Anwendung eines nachhaltigen Unverpackt-Lieferservice
(2022)
Die Welt wird wortwörtlich von Plastik überschwemmt- und trotzdem ist kein Ende des trivialen Verpackungsmaterials in Sicht. Die, die sich den Konsequenzen ihres Konsumverhaltens bewusst sind, haben immer noch keinen flächendeckenden Zugang zu Unverpacktläden und es mangelt schlicht an praktischen Alternativen.
Hier knüpft die App „bulk“ an und schlägt ausschließlich unverpackte Lebensmittel vor – bequem bis zur Haustür geliefert. Das Angebot ist qualitativ hochwertig und meist regional. Für ein positives Kauferlebnis veranschaulicht „bulk“, wie viel Plastik mit den Produkten im Vergleich zu einem konventionellen Wocheneinkauf eingespart werden kann. Das gibt Nutzer:Innen eine Grundlage, ihre Entscheidungen kritisch zu hinterfragen und schult den Blick für den Impact sich summierender Kleinigkeiten.
Ländliche Regionen sind häufig infrastrukturell schlechter versorgt als urbane Räume, was sich insbesondere auf die Versorgung mit Gütern des täglichen Bedarfs niederschlägt. Menschen außerhalb städtischer Ballungsgebiete müssen deswegen oft lange Anfahrten zu Supermärkten in Kauf nehmen. Hierbei sind sie vor allem auf das Auto angewiesen.
In dieser Arbeit ist „ILSE“ entstanden. Eine Verkaufsbox, die Menschen in ländlichen Raumstrukturen besser mit Waren versorgt, indem sie dort aufgestellt wird, wo sie auch wirklich benötigt wird.
Dank digitaler Verkaufstechnologien ist „ILSE“ durchgehend geöffnet, auch, wenn andere Supermärkte längst geschlossen sind. Mit einer App wird der Kundschaft der Zugang zum Verkaufsraum und das Bezahlen ermöglicht.
In dieser Arbeit wurde sich mit der Frage auseinandergesetzt, wie sich der Nahrungsmittelanbau im urbanen Raum entwickeln könnte. Eine spannende Alternative zu traditionellen Anbaumethoden ist die Hydroponik, der Anbau von Pflanzen ohne Erde. Basierend auf dieser Technologie wurde in diesem Projekt ein Indoor-Garden-System gestaltet, welches den Nahrungsmittelanbau zurück zur Verbraucher:In bringt und zu einem bewussteren Umgang mit Lebensmitteln anregen soll.
Denn mit „INGA“ kann frisches, pestizidfreies Blattgemüse ganz einfach zu Hause selbst angebaut werden. Das hydroponische System schafft mithilfe einer Nährstofflösung und künstlichem Licht optimale Wachstumsbedingungen für die Pflanzen – ganz unabhängig von örtlichen Gegebenheiten. Mithilfe seiner Modularität können Nutzer:Innen „INGA“ nach Belieben konfigurieren. Damit wird es einer breiten Zielgruppe mit unterschiedlichen Bedürfnissen gerecht und ermöglicht pestizidfreie Nahrung – auch in den Städten.
This paper describes the results and methods used during the 8th Global Trajectory Optimization Competition (GTOC) of the DLR team. Trajectory optimization is crucial for most of the space missions and usually can be formulated as a global optimization problem. A lot of research has been done to different type of mission problems. The most demanding ones are low thrust transfers with e.g. gravity assist sequences. In that case the optimal control problem is combined with an integer problem. In most of the GTOCs we apply a filtering of the problem based on domain knowledge.
Unterhaltungsgegenstände und ihre Add-Ons stellen für viele Menschen ein wichtiger Bestandteil eines ausgewogenen Lebens dar und sind somit nicht mehr aus klassischen Haushalten wegzudenken. Doch nicht jeder Menschen hat überhaupt Zugang zu ihnen, weil die Systeme meistens auf Durchschnittsbürger:Innen abgestimmt sind. Davon betroffen sind beispielsweise Menschen mit Blindheit und Seheinschränkung. Um das Angebot individueller zu gestalten, wurde diesem Projekt ein Home-Entertainment-System entwickelt, das eben genau auf die Bedürfnisse dieser Gruppe zugeschnitten ist. Für die bedienungsfreundliche Gestaltung wurde im gesamten Prozess besonders viel Wert auf die konkrete Lebensrealität von Blinden und Menschen mit Seheinschränkungen gelegt. Hier sollen mögliche Einschränkungen überwunden werden und sich möglichst den tatsächlichen Anforderungen in der Praxis anpassen.
Dazu musste zunächst ein umfassendes Verständnis des Krankheitsbildes geschult werden. Außerdem wurde ein Blick in den Alltag dieser Menschen geworfen. Welche Home-Entertainmentgeräte finden bereits im Wohnzimmer Platz und welche Komplikationen gibt es mit ihnen? Die breite Palette an Produkten gibt einen Eindruck davon, welche Funktionen ersetzt und welche Systeme gegebenenfalls miteinander verknüpft werden können.
Auf der Basis umfassender Recherche ist eine Fernbedienung entstanden, die sowohl per Sprachsteuerung als auch über physische Steuerung steuerbar ist. Zahlreiche taktile Elemente geben Orientierung bei der Nutzung und gewährleisten ein reibungsloses und handliches Nutzungserlebnis. Die Arbeit öffnet den Blick für andere Lebenswelten und plädiert für den Abbau von Barrieren für ein selbstbestimmteres Leben.