Small Projects
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For Delta-Utec's involvement in ESA's study on Cultural Utilisation of the ISS, please see: Alexander van Dijk
Support to Smart 1: Optimization of low thrust trajectories
Delta-Utec has developed and acquired several optimization tools. One of them is a genetic algorithm optimizer, developed by Robin Biesbroek. In this support project to Smart 1, an optimal control law for low thrust escape trajectories analytically derived by F. Janssens (ESA/ESTEC) was evaluated. The investigation has led to a support of Janssens' conclusion that even for escape trajectories, with a rapidly increasing semi-major axis, a simple tangential thrust direction provides (near)-optimal results.
Support to LunarSat: Asteroid rendez-vous with low thrust engines
In support of the feasibility study for science targets of LunarSat successors, Delta-Utec has developed an orbit integrator and simulator suitable for simultaneous integration and optimization of rendez-vous or fly-by options to an unlimited number of asteroids, with the option to use genetic algorithms. The model includes low thrust option and the possibility to force planetary swing-by's and/or Weak Stability Boundary solutions to be part of the solution. An unlimited number of parameters can be part of the optimization, allowing great freedom in the definition of the thrust program.

Simulation of WSB and Earth/Moon swing-bys
Of course, Sun and Moon ephemeris, J2-gravity anomaly and an option for launch time selection is included. A graphical output makes a quick interpretation possible of the orbits found.
Support to EuroMoon: Lunar landing site investigations
Recent missions to the moon, Clementine & Lunar Observer, have put forward the lunar poles as a major target for interplanetary travel. Already predicted by a number of publications, it has finally been generally accepted that these poles have three great advantages for human exploration and scientific interest:
A paper by Delft University of Technology, Delta-Utec and ESTEC for the first time has pinned down these Peaks of Eternal Light on the lunar South Pole and has developed a method for obtaining a three-dimensional profile of these sites, as well as a method to discover the Peaks of Eternal Light on the lunar North Pole, from the small amount of data currently available.
The research has been updated in July 2000 for the ICEUM 4 conference at ESA/ESTEC. Download here.
The Peaks of Eternal Light at the lunar South Pole
Activities initiated at ESTEC by Delta-Utec engineering, i.e.
have been pursued for EuroMoon by a student from Delft University of Technology, J.F. de Weerd, currently employed by Libertel.
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A synthetic lunar day at the South Pole: fully simulated!
As part of the Delta-Utec R&D program, De Weerd's work has been finalized and documented. His work has resulted in a new set of tools for lunar landing mission planning:
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Monthly Illumination Spectra : a powerful tool to determine how much Sunlight any site on the lunar poles receives in time, that can also be used to estimate surface profiles and pin down Peaks of Eternal light, all this from typical polar orbiter images. This tool can be used on the Lunar North Pole and the equally interesting poles of Mercury. |
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First physical 3D model (scale 1:300) and digital elevation map of lunar South Pole surface. The model has been extensively used for demonstration and planning purposes and was produced in a particularly creative way, by simulating the light source and shadowing on a wax clay model. |
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Lunar surface simulator for interactive landing trajectory simulations :A landing on a Peak of Eternal Light requires pinpoint accuracy. This can only be reached if there's intelligent interaction with a camera, taking images of the surface, and an operator: either machine or Earth based human controller. Both will have to practise their skills of recognizing the lunar fractal like surface. This tool simulates the lighting, shadowing and scattering of the lunar surface, as well as the fractal effect of small craters and surface roughness, appearing on approach. |