Abstract: A propellant ignition testing apparatus having a compressively sealable chamber. A fixed end plate assembly is fixedly mounted on a support structure. A test chamber assembly having a combustion chamber for accommodating propellant is provided, and an initiator ignites propellant accommodated in the combustion chamber. A moveable end plate is disposed adjacent to the test chamber assembly on a side thereof remote from the fixed end plate assembly. A device is mounted on the support structure for generating a compressive force, with the moveable end plate being operatively connected to a moveable component of the device for moving the moveable end plate toward the test chamber assembly for sandwiching the combustion chamber of the test chamber assembly in a compressively sealed manner between the fixed end plate assembly and the moveable end plate.

Abstract: A propellant ignition testing apparatus having a compressively sealable chamber. A fixed end plate assembly is fixedly mounted on a support structure. A test chamber assembly having a combustion chamber for accommodating propellant is provided, and an initiator ignites propellant accommodated in the combustion chamber. A moveable end plate is disposed adjacent to the test chamber assembly on a side thereof remote from the fixed end plate assembly. A device is mounted on the support structure for generating a compressive force, with the moveable end plate being operatively connected to a moveable component of the device for moving the moveable end plate toward the test chamber assembly for sandwiching the combustion chamber of the test chamber assembly in a compressively sealed manner between the fixed end plate assembly and the moveable end plate.

Abstract: A method of aligning an inertial navigation system or gyrocompass, including executing real-time navigation software on real-time inertial data to generate real-time navigation data, executing real-time Kalman filter software on the real-time navigation data and real-time aiding data, recording the real-time inertial data and the real-time aiding data as real-time input data in a buffer, initializing a playback process, executing playback navigation software on buffered inertial data to generate playback navigation data, and executing playback Kalman filter software on the playback navigation data and buffered aiding data. The execution of the real-time navigation software and the real-time Kalman filter software effect a real-time alignment process. The playback navigation software and the playback Kalman filter software effect an alignment process executed at a faster rate than the real-time navigation software and real-time Kalman filter software.

Abstract: A method of aligning a gyro-compass comprising operating at least two Kalman filters in a set of Kalman filters to generate an error correction to at least a single navigation solution in a set of navigation solutions in order to provide coarse alignment azimuth convergence. The method further comprises selecting at least one selected Kalman filter from the set of Kalman filters and at least one selected navigation solution from the set of navigation solutions, and operating the at least one selected Kalman filter and the at least one selected navigation solution to provide fine alignment convergence to a correct azimuth. The selecting is based at least in part on the generated error correction, each navigation solution includes an azimuth different from the azimuth of each other navigation solution and each navigation solution azimuth is separated by no more than two times a small angle error assumption.

Abstract: A method of aligning an inertial navigation system or gyrocompass, including executing real-time navigation software on real-time inertial data to generate real-time navigation data, executing real-time Kalman filter software on the real-time navigation data and real-time aiding data, recording the real-time inertial data and the real-time aiding data as real-time input data in a buffer, initializing a playback process, executing playback navigation software on buffered inertial data to generate playback navigation data, and executing playback Kalman filter software on the playback navigation data and buffered aiding data. The execution of the real-time navigation software and the real-time Kalman filter software effect a real-time alignment process. The playback navigation software and the playback Kalman filter software effect an alignment process executed at a faster rate than the real-time navigation software and real-time Kalman filter software.

Abstract: A method of aligning a gyro-compass comprising operating at least two Kalman filters in a set of Kalman filters to generate an error correction to at least a single navigation solution in a set of navigation solutions in order to provide coarse alignment azimuth convergence. The method further comprises selecting at least one selected Kalman filter from the set of Kalman filters and at least one selected navigation solution from the set of navigation solutions, and operating the at least one selected Kalman filter and the at least one selected navigation solution to provide fine alignment convergence to a correct azimuth. The selecting is based at least in part on the generated error correction, each navigation solution includes an azimuth different from the azimuth of each other navigation solution and each navigation solution azimuth is separated by no more than two times a small angle error assumption.