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

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Chapter 4.0 Entomopter Flight Operations<br />

4.1 Entomopter Navigation and Communications on Mars<br />

Chapter 4.0 Entomopter Flight Operations<br />

4.1 Entomopter Navigation and Communications on<br />

Mars<br />

There are presently no global navigation systems on Mars to support an Entomopter-based aerial<br />

survey mission. Although such a network may be established in the future, it is not really essential<br />

to the Entomopter navigation function. Because Entomopters are designed to return to the<br />

rover base <strong>for</strong> refueling, their operations are necessarily rover-centric. For this reason, all navigation<br />

cues can (and probably should) be referenced to the refueling rover's position, which<br />

from the Entomopter's perspective is decoupled from any Mars coordinate system. All the Entomopters<br />

need to know is where they are relative to the refueling rover. The refueling rover, on<br />

the other hand, should have an awareness of its global position, but this position is largely irrelevant<br />

to the Entomopters. This is particularly true because Entomopter missions are planned to be<br />

local to the rover. Due to endurance constraints, the Entomopters are not envisioned as striking<br />

out across the Mars landscape to investigate points hundreds of kilometers distant.<br />

This section will present two approaches to Entomopter navigation and communication. The two<br />

differ in terms of architecture- basically, where emitters are located. In one case, most of the<br />

emitters are carried by the refueling rover, and except <strong>for</strong> a short distance low-power ranging<br />

device to aid in landing, the Entomopters are free from the weight burden of this support equipment.<br />

The other option presented places various emitters on the Entomopters, the advantage<br />

being that longer range operation is possible and non-line-of-sight flight (relative to the refueling<br />

rover) is simplified. The price to be paid <strong>for</strong> this increase in per<strong>for</strong>mance is decreased science<br />

payload capacity in terms of weight and volume when both emitters and their supporting<br />

energy source are considered. The particular science mission goal will dictate which method is<br />

preferred.<br />

4.2 Rover-centric Entomopter Navigation<br />

Because the refueling rover (by definition) is replete with fuel and is there<strong>for</strong>e not energy constrained<br />

to the degree that a flying vehicle would be, it has the luxury of emitting relatively high<br />

power radio frequency (RF) radiation (a costly behavior due to emitter inefficiencies). As such,<br />

the rover can support a radar system capable of detecting and tracking objects within a hemispherical<br />

volume centered about the rover.<br />

The Entomopter has a distinctive radar cross-section (RCS) that involves both high frequency<br />

local motions and translational motions. Doppler target acquisition and tracking radar on the<br />

rover would easily identify Entomopters in flight based on their motion as distinguished from<br />

the stationary Mars landscape. The wingbeat would provide a high frequency (10s of Hz) modulation<br />

of the RCS in terms of amplitude, while the flight speed of the Entomopter would provide<br />

a Doppler shift of magnitude and sign that depends upon angle of approach or departure. Additionally,<br />

the elevation of the Entomopters would be a discriminator most of the time as well, so<br />

long as they were operating in the general vicinity of the rover.<br />

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