Localization and Observability of Aircraft via Doppler Shifts
The linear trajectory of an airplane with constant velocity is obtained from Doppler shifts at stationary sensors, each yielding a corresponding time of closest approach, closest distance, and speed [3, 8]. Based on these inferences and on the sensors' locations, three sensors yield two candida...
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| Veröffentlicht in: | IEEE transactions on aerospace and electronic systems 2007-07, Vol.43 (3), p.1163-1168 |
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| container_title | IEEE transactions on aerospace and electronic systems |
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| creator | Torney, D.C. |
| description | The linear trajectory of an airplane with constant velocity is obtained from Doppler shifts at stationary sensors, each yielding a corresponding time of closest approach, closest distance, and speed [3, 8]. Based on these inferences and on the sensors' locations, three sensors yield two candidate trajectories, and four sensors yield one - provided that the locations span R 2 and R 3 respectively: constituting observability for the problem at hand. |
| doi_str_mv | 10.1109/TAES.2007.4383606 |
| format | Article |
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| language | eng |
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| source | IEEE Electronic Library (IEL) |
| subjects | Aircraft Aircraft components Airplanes Computer networks Doppler effect Doppler radar Doppler shift Electronic systems Equations Frequency Localization Observability Sensors Tactile sensors Trajectories Vectors |
| title | Localization and Observability of Aircraft via Doppler Shifts |
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