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In this case, a reorientation maneuver is necessary to follow the optimal thrust direction.
The required optimal thrust magnitude and direction can be determined to create the bridging trajectory that connects the invariant manifolds.
Modern military aircraft jet engines are designed with variable-geometry nozzles to provide optimal thrust in different operating conditions, depending on the flight envelope.
A Dynamic Positioning System (DPS) is a complex control system composed of several algorithms, such as controllers, filters and optimal thrust allocation.
The optimal thrust solution typically has a "bang-bang" profile considering that bounds are imposed on the magnitude of engine thrust.
The effects of electrodes distance and the off-axis distance between ceramic tube and cathode were tested, and it׳s found that there were optimal structural parameters for achieving optimal thrust performance.
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Low-thrust optimisation is then performed to turn bi-impulse transfers into optimal low-thrust transfers, and refine the selected scenarios.
In this guidance scheme, the ANN is adopted to determine the burn structure within each orbital revolution and the optimal low-thrust orbit transfer problem is converted to the parameter optimization problem.
It is difficult and time-consuming to search the optimal low-thrust spiral trajectories.
However, it is particularly challenging to search for optimal low-thrust transfers.
The search for the globally optimal, low-thrust, gravity-assist trajectory for maximally deflecting an asteroid is performed in two steps.
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Justyna Jupowicz-Kozak
CEO of Professional Science Editing for Scientists @ prosciediting.com