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<!DOCTYPE HTML PUBLIC "-//W3C//DTD HTML 4.01//EN" "http://www.w3.org/TR/html4/strict.dtd"> <html> <head> <title>page_232</title> <link rel="stylesheet" href="reset.css" type="text/css" media="all"> <meta http-equiv="Content-Type" content="text/html; charset=UTF-8" /> </head> <body> <table summary="top nav" border="0" width="100%"> <tr> <td align="left" width="30%" style="background: #EEF3E2"><a style="color: blue; font-size: 120%; font-weight: bold; text-decoration: none; font-family: verdana;" href="page_231.html">< previous page</a></td> <td id="ebook_previous" align="center" width="40%" style="background: #EEF3E2"><strong style="color: #2F4F4F; font-size: 120%;">page_232</strong></td> <td align="right" width="30%" style="background: #EEF3E2"><a style="color: blue; font-size: 120%; font-weight: bold; text-decoration: none; font-family: verdana;" href="page_233.html">next page ></a></td> </tr> <tr> <td id="ebook_page" align="left" colspan="3" style="background: #ffffff; padding: 20px;"> <table border="0" width="100%" cellpadding="0"><tr><td align="center"> <table border="0" cellpadding="2" cellspacing="0" width="100%"><tr><td align="left"></td> <td align="right"></td> </tr></table></td></tr><tr><td align="left"><p></p><table border="0" cellspacing="0" cellpadding="0" width="100%"><tr><td align="right"><font face="Times New Roman, Times, Serif" size="2" color="#FF0000">Page 232</font></td></tr></table><table border="0" cellspacing="0" cellpadding="0"><tr><td rowspan="5"></td> <td colspan="3" height="12"></td> <td rowspan="5"></td></tr><tr><td colspan="3"></td></tr><tr><td></td> <td><font face="Times New Roman, Times, Serif" size="3"><i>6.8.2<br />Aided Initialization and Error Estimation</i></font></td><td></td></tr><tr><td colspan="3"></td></tr><tr><td colspan="3" height="1"></td></tr></table><table border="0" cellspacing="0" cellpadding="0"><tr><td rowspan="5"></td> <td colspan="3" height="12"></td> <td rowspan="5"></td></tr><tr><td colspan="3"></td></tr><tr><td></td> <td><font face="Times New Roman, Times, Serif" size="3">In many applications, instruments sufficient to enable accurate self-initialization cannot be justified because of their high cost. For these application, many forms of aided initialization and error estimation are available: optical measurements, master-slave, GPS, radar, and starting at rest at a known initial location.</font></td><td></td></tr><tr><td colspan="3"></td></tr><tr><td colspan="3" height="1"></td></tr></table><table border="0" cellspacing="0" cellpadding="0"><tr><td rowspan="5"></td> <td colspan="3" height="12"></td> <td rowspan="5"></td></tr><tr><td colspan="3"></td></tr><tr><td></td> <td><font face="Times New Roman, Times, Serif" size="3">Equation (6.155) is valid for any three independent vectors. Optical sightings are sometimes used to replace one of the three vectors in that equation. Otherwise the procedure is identical.</font></td><td></td></tr><tr><td colspan="3"></td></tr><tr><td colspan="3" height="1"></td></tr></table><table border="0" cellspacing="0" cellpadding="0"><tr><td rowspan="5"></td> <td colspan="3" height="12"></td> <td rowspan="5"></td></tr><tr><td colspan="3"></td></tr><tr><td></td> <td><font face="Times New Roman, Times, Serif" size="3">Master-slave initialization uses one accurate, previously initialized INS to calibrate a second INS. The second INS may have been recently turned on or of low enough quality that significant drift is expected to have occurred since the last calibration. This case is common for the initialization of position and velocity in missile INS applications, in which an expensive INS is not warranted because of the short span of time over which accurate postlaunch navigation is required and because of the expectation that the INS will be destroyed with the missile. Master-slave initialization may take a variety of forms. In a one-shot alignment (or transfer alignment) the state of the master INS is used to initialize the state of the slave INS at a particular instant of time. Alternatively, the position, velocity, or inertial measurements of the master INS could be differenced with the same quantities of the slave INS. The resulting residual measurements drive a Kalman-filter-based error estimator [11].</font></td><td></td></tr><tr><td colspan="3"></td></tr><tr><td colspan="3" height="1"></td></tr></table><table border="0" cellspacing="0" cellpadding="0"><tr><td rowspan="5"></td> <td colspan="3" height="12"></td> <td rowspan="5"></td></tr><tr><td colspan="3"></td></tr><tr><td></td> <td><font face="Times New Roman, Times, Serif" size="3">These filter-based approaches are discussed in the subsequent sections. Aided initialization and error estimation methods are complicated by the fact that the aiding system and the INS are separated by a lever arm (see Sec. 6.9). The lever-arm length and alignment may not be accurately known because of manufacturing tolerances, different possible system locations (i.e., missiles in different positions), lever-arm flex, and vibration. Lever-arm and disturbance effects must be accounted for if accurate error estimation is to be expected.</font></td><td></td></tr><tr><td colspan="3"></td></tr><tr><td colspan="3" height="1"></td></tr></table><table border="0" cellspacing="0" cellpadding="0"><tr><td rowspan="5"></td> <td colspan="3" height="12"></td> <td rowspan="5"></td></tr><tr><td colspan="3"></td></tr><tr><td></td> <td><font face="Times New Roman, Times, Serif" size="3">If the aided INS is configured in feedback form, then the aiding signal can be used as the first Kalman filter measurement. The correction, in this case the initial state, is fed back to initialize the INS. The process is similar to that described in the following subsections and is not repeated here. A stochastic model of the error in the aiding signal is required so that the Kalman filter can accurately account for the error variance propagation.</font></td><td></td></tr><tr><td colspan="3"></td></tr><tr><td colspan="3" height="1"></td></tr></table><table border="0" cellspacing="0" cellpadding="0"><tr><td rowspan="5"></td> <td colspan="3" height="12"></td> <td rowspan="5"></td></tr><tr><td colspan="3"></td></tr><tr><td></td> <td><font face="Times New Roman, Times, Serif" size="3">In each of the following subsections issues are discussed that are related to solving the estimation problem from a given class of measurements. The analysis will show that the observability of the estimation problem is application and trajectory dependent. For simplicity of presentation in the subsequent analysis, the error dynamics will neglect the altitude states. Inclusion of these states does not change the overall observability conclusions, but would alter the numeric results. This decoupling is physically motivated in low dynamic situations.</font><font face="Times New Roman, Times, Serif" size="3" color="#FFFF00"></font></td><td></td></tr><tr><td colspan="3"></td></tr><tr><td colspan="3" height="1"></td></tr></table></td></tr></table><p><font size="0"></font></p>聽 </td> </tr> <tr> <td align="left" width="30%" style="background: #EEF3E2"><a style="color: blue; font-size: 120%; font-weight: bold; text-decoration: none; font-family: verdana;" href="page_231.html">< previous page</a></td> <td id="ebook_next" align="center" width="40%" style="background: #EEF3E2"><strong style="color: #2F4F4F; font-size: 120%;">page_232</strong></td> <td align="right" width="30%" style="background: #EEF3E2"><a style="color: blue; font-size: 120%; font-weight: bold; text-decoration: none; font-family: verdana;" href="page_233.html">next page ></a></td> </tr> </table> </body> </html>⌨️ 快捷键说明
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