Introduction I NVESTIGATIONS into the application of inertial technology to geodetic surveys have covered a span of at least 25 years, involving a number of private companies and government and university laboratories. The principal agency sponsoring this work in the United States has been the U.S. Army Engineer Topographic Laboratories (USAETL), whose original efforts began in the early 1960s. In 1965 the Guidance and Control Systems Division of Litton Industries began its initial tradeoff studies on the Position and Azimuth Determining System (PADS) under USAETL sponsorship. The original estimation problem posed for the PADS was to design software to process discrete measurements from an odometer, or a laser-velocimeter, of the error in systemcomputed velocity observable at vehicle stops (subsequently called Zero-Velocity Updates or ZUPTS), so that accuracies of 20 m in level position, 10 m in elevation, and 0.3 mrad in azimuth were preserved over a 6-h open-traverse mission. The solution obtained was that of two independent Kalman filters, one for control of the errors associated with the local-level navigation axes and the other for control of errors associated with the vertical axis. Periodic vehicle stops were required, depending on the mode of system operation, to make system corrections with the Kalman filter(s) of the observed velocity error. The design was verified for all three modes of operation via simulation with extensive system error models and successfully field-tested in 1972. The first paper available to the general public on the basic principles for control of system error in the design of the PADS, along with simulation and test results was published in the same year. As in practice the stopping of the vehicle every 10 min to make ZUPT corrections 4s not excessively inconvenient, the principal operational mode for the PADS has become the unaided, free-inertial mode during vehicle travel. Also contributing to this result was the fact that the laser-velocimeter was an expensive sensor which gave the vehicle a distinctive signature, although it allowed the travel period to be extended to 1 h. Utilization of the odometer has also diminished as it extended the travel period to only 20 min. The success of the PADS prototype hardware-testing program for the free-inertial mode in 1972' stimulated interest by a number of groups on the utilization of this inertial equipment for a higher-accuracy position, elevation, and gravityvector survey capability in helicopters as well as land vehicles. The higher accuracy was easily obtained by relaxing the constraints imposed by the real-time artillery survey mission. The techniques employed were longer pre-mission alignment and calibration time, shorter travel periods between vehicle stops, longer stop periods during which system corrections of the observed error in system-computed velocity were made, and simple adjustment of the real-time position and elevation survey values, using the errors in these quantities available (only) at traverse closure.''
Read full abstract