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Two stepper motors were used for controlling the descent phase.
This paper proposes the MCAV/IMU integrated navigation scheme for the powered descent phase of Mars EDL.
In this paper, the Zero-Effort-Miss/Zero-Effort-Velocity (ZEM/ZEV) optimal sliding guidance (OSG) scheme is applied to the Mars powered descent phase.
Backpropagation gives the best accuracy for the climb and cruise phases, whereas the Levenberg Marquardt algorithm is optimal for the descent phase.
The approach aims to detect craters on the planetary surface and match them to a landmark database during the descent phase of a planetary landing mission.
This paper deals with one aspect of the pinpoint landing architecture the navigation performance improvement during the powered descent phase, and proposes an innovative navigation scheme to obtain the vehicle complete and accurate states.
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Next, the state-of-art guidance technologies of entry and powered descent phases are analyzed.
Results showed significant differences in both ascent and descent phases post-intervention indicating changes in the movement programme.
The safety index can be applied in various planetary descent phases and provides reference for future mission designs.
A minimum of 5 km was chosen due to the 2.5 km horizontal slant range during both climb and descent phases.
Finally, due to the cruise altitude of 1000 ft and the assumed rate of climb (ROC) and rate of descent (ROD) of 1000 fpm, the climb and descent phases have a duration of only 2 min, which is only a small portion of the 25 min flight in the base case.
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