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Integrated Systems and their Impact on the Future of Positioning ...

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maps will be c<strong>on</strong>sidered for l<str<strong>on</strong>g>and</str<strong>on</strong>g> vehicle navigati<strong>on</strong>, <str<strong>on</strong>g>and</str<strong>on</strong>g> pedometers, magnetic<br />

compasses, digital maps, <str<strong>on</strong>g>and</str<strong>on</strong>g> cellular ph<strong>on</strong>es for backpack systems.<br />

The integrati<strong>on</strong> <strong>of</strong> <strong>the</strong> navigati<strong>on</strong> technologies (GPS, INS, <str<strong>on</strong>g>and</str<strong>on</strong>g> visi<strong>on</strong>-based<br />

technologies) with navaids provides a system that has superior performance in<br />

comparis<strong>on</strong> with ei<strong>the</strong>r a GPS, an INS, or visi<strong>on</strong>-based st<str<strong>on</strong>g>and</str<strong>on</strong>g>-al<strong>on</strong>e system. For<br />

instance, GPS derived positi<strong>on</strong>s have approximately white noise characteristics over <strong>the</strong><br />

whole frequency range. The GPS-derived positi<strong>on</strong>s <str<strong>on</strong>g>and</str<strong>on</strong>g> velocities are <strong>the</strong>refore<br />

excellent external measurements for updating <strong>the</strong> INS <str<strong>on</strong>g>and</str<strong>on</strong>g> providing <strong>the</strong> imaging<br />

sensors with positi<strong>on</strong> parameters, thus improving its l<strong>on</strong>g-term accuracy. Similarly, <strong>the</strong><br />

INS can provide precise positi<strong>on</strong> <str<strong>on</strong>g>and</str<strong>on</strong>g> velocity data for GPS signal acquisiti<strong>on</strong> <str<strong>on</strong>g>and</str<strong>on</strong>g><br />

reacquisiti<strong>on</strong> after outages <str<strong>on</strong>g>and</str<strong>on</strong>g> <strong>the</strong> orientati<strong>on</strong> parameters for <strong>the</strong> visi<strong>on</strong>-based system.<br />

The visi<strong>on</strong>-based system can be used as a backup navigati<strong>on</strong> system <str<strong>on</strong>g>and</str<strong>on</strong>g> to update <strong>the</strong><br />

INS data if <strong>the</strong> GPS signal is blocked for l<strong>on</strong>g periods. In general, <strong>the</strong> fact that<br />

redundant measurements are available for <strong>the</strong> determinati<strong>on</strong> <strong>of</strong> <strong>the</strong> vehicle trajectory<br />

parameters greatly enhances <strong>the</strong> reliability <strong>of</strong> <strong>the</strong> system.<br />

The navigati<strong>on</strong> states vector (positi<strong>on</strong>, velocity, <str<strong>on</strong>g>and</str<strong>on</strong>g> attitude) can be determined by<br />

judicially combining elements <strong>of</strong>: navigati<strong>on</strong> technologies (e.g. GPS, Inertial, <str<strong>on</strong>g>and</str<strong>on</strong>g><br />

visi<strong>on</strong>-based) <str<strong>on</strong>g>and</str<strong>on</strong>g> navigati<strong>on</strong> aids (e.g. distance, velocity, <str<strong>on</strong>g>and</str<strong>on</strong>g> attitude sensors). This is<br />

shown in Figure (2) where <strong>the</strong> navigati<strong>on</strong> technologies <str<strong>on</strong>g>and</str<strong>on</strong>g> navaids are listed in two<br />

blocks. Table (1) lists current <str<strong>on</strong>g>and</str<strong>on</strong>g> possible integrated systems scenarios. Table (2) lists<br />

which sub-vectors <strong>of</strong> <strong>the</strong> Navigati<strong>on</strong> State that can be obtained with <strong>the</strong>se systems<br />

scenarios <str<strong>on</strong>g>and</str<strong>on</strong>g> which characteristics <str<strong>on</strong>g>and</str<strong>on</strong>g> <strong>the</strong> resulting integrated system will have.<br />

Possible applicati<strong>on</strong>s are <strong>the</strong>n given in <strong>the</strong> last column.<br />

The Tables indicate that a wide variety <strong>of</strong> integrati<strong>on</strong> strategies can be implemented.<br />

Each has its own characteristics <str<strong>on</strong>g>and</str<strong>on</strong>g> <strong>the</strong> choice <strong>of</strong> a specific system will be based <strong>on</strong><br />

system requirements <str<strong>on</strong>g>and</str<strong>on</strong>g> applicati<strong>on</strong>s. Although it is possible to integrate any set <strong>of</strong><br />

technologies, <strong>the</strong> integrati<strong>on</strong> <strong>of</strong> GPS <str<strong>on</strong>g>and</str<strong>on</strong>g> INS represents <strong>the</strong> core <strong>of</strong> for any integrated<br />

systems where reliability <str<strong>on</strong>g>and</str<strong>on</strong>g> versatility are <strong>the</strong> major issues. The low cost <strong>of</strong> GPS<br />

receivers, <strong>the</strong> coverage <str<strong>on</strong>g>and</str<strong>on</strong>g> reliability <strong>of</strong> GPS, <str<strong>on</strong>g>and</str<strong>on</strong>g> <strong>the</strong> expected decrease in cost <strong>of</strong><br />

MEMS-based inertial sensors make GPS <str<strong>on</strong>g>and</str<strong>on</strong>g> INS <strong>the</strong> logical technologies for realizing<br />

<strong>the</strong> benefits <strong>of</strong>fered by integrated positi<strong>on</strong>ing systems. Many companies are currently<br />

working <strong>on</strong> <strong>the</strong> integrati<strong>on</strong> <strong>of</strong> MEMS based IMU with GPS, with projecti<strong>on</strong>s <strong>of</strong> size,<br />

weight <str<strong>on</strong>g>and</str<strong>on</strong>g> power at 2 x 2 x 0.5 cm, 5 g, <str<strong>on</strong>g>and</str<strong>on</strong>g> less than 1 W for implementati<strong>on</strong> at <strong>the</strong><br />

ASIC level. Figure 3, shows typical performances for some <strong>of</strong> <strong>the</strong> scenarios listed in<br />

Table 1.

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