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1116results about How to "Simple requirements" patented technology

Interface for translating an information message from one protocol to another

A computer implemented interface for interfacing an equipment controller to an equipment manager each arranged to respond to a reproduced text messages according to a first and second protocol, respectively. The interface comprises a number of program modules (502-514) which each receive one or more inputs and produce an output dependent on whether defined conditions are met by the inputs. A number of the outputs of the program modules constitute inputs to other program modules therefore defining a network. A number of the program modules (502-508) are of the type which is responsive to a predefined text in a respective field of an input message to produce an output to a further program module which is responsive to a further predefined text in another field which is valid in a first protocol in the context of the predefined text. The network of program modules produces a series of outputs which represent the information content of the original input message. These outputs are then passed to a further series of modules which format a translation of the input message. The defined conditions of the program modules are modifiable and in particular are modifiable in a manner which is dependent on the state of part of the equipment management system thereby providing an inherent model of the network management system for use during parsing of an input message.
Owner:BRITISH TELECOMM PLC

Double-shaft continuous rotation-based hybrid type platform inertial navigation system calibration method

The invention discloses a double-shaft continuous rotation-based hybrid type platform inertial navigation system calibration method. The method comprises the following steps: (1) performing coarse alignment to obtain a coarse initial attitude matrix; (2) controlling an outer ring shaft and a platform body shaft of a platform system to rotate at the same angular speed, enabling an inner ring shaftto be under a locked state, and acquiring gyroscope and accelerometer output in the rotating process; (3) resolving an error state equation and an observation equation and calibrating gyroscope scalefactor error, gyroscope mounting error and accelerometer equivalent zero offset; (4) controlling an outer ring frame angle, an inner ring frame angle and a platform body frame angle to lock in a zerostate, rotating the platform body shaft by 180 degrees and locking, and acquiring output data of the gyroscope; (5) controlling the outer ring frame angle, the inner ring frame angle and the platformbody frame angle to lock in the zero state, rotating the outer ring shaft by 180 degrees and locking, and acquiring output data of the gyroscope; and (6) calculating the constant drift of the gyroscope. By the method, the calibration time is effectively shortened and the calibration efficiency is improved.
Owner:BEIJING INST OF AEROSPACE CONTROL DEVICES
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