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Phase II Final Report - NASA's Institute for Advanced Concepts

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Planetary Exploration Using Biomimetics<br />

An Entomopter <strong>for</strong> Flight on Mars<br />

Figure 2-4: Integral Propulsion-ultrasonic Obstacle Avoidance and Altimetry System<br />

Motivation <strong>for</strong> navigation would be based on various remote sensors that will be dictated by the<br />

type of science experiments to be per<strong>for</strong>med by each Entomopter. For example, the search <strong>for</strong><br />

life might entail sensors that can detect traces of water or fossil-bearing rock. Other Mars Flyers<br />

could measure atmospheric species or per<strong>for</strong>m reconnaissance <strong>for</strong> later close inspection by<br />

ground-based rovers. In each case, the Mars Flyers would use preprogrammed search patterns<br />

initially. When measuring a volume, as in the case of atmospheric sampling, the entire flight<br />

might be preprogrammed. When searching <strong>for</strong> life, a preprogrammed search pattern would be<br />

abandoned in favor of following gradients based on the frequency of occurrence of evidence<br />

(motivational behavior). During the landing process, obstacles on the surface must be negotiated<br />

(avoidance behavior), and the Entomopter must select a spot from which it can launch itself<br />

back into the air as it transitions from ground locomotion to flight.<br />

Due to the occurrence of storms on Mars, the Entomopter-based Mars Flyers might have to seek<br />

shelter on the surface by landing in a self preservation behavior. In all cases however, the Mars<br />

Flyers would have to be able to find their way back to the lander or rover in order to replenish<br />

depleted fuel supplies as they exhibit a feeding behavior also driven by a self preservation motivation.<br />

The ability to fly autonomously is possible because of the ability of the Entomopter to modulate<br />

its coefficient of lift <strong>for</strong> each wing section on a beat-to-beat basis, thereby controlling attitude.<br />

This feature also permits the vehicle to change heading <strong>for</strong> navigation. Implicit is the presence<br />

of an onboard inertial system having stability that is either of duration commensurate with the<br />

flight mission length, or that is updated by an external reference analogous to GPS.<br />

28<br />

<strong>Phase</strong> <strong>II</strong> <strong>Final</strong> <strong>Report</strong>

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