Add to ORKGResults of flight tests of the Strapdown Inertial Reference Unit (SIRU) navigation system are presented. The fault tolerant SIRU navigation system features a redundant inertial sensor unit and dual computers. System software provides for detection and isolation of inertial sensor failures and continued operation in the event of failures. Flight test results include assessments of the system's navigational performance and fault tolerance. Performance shortcomings are analyzed
Proposed testing program for strapdown inertial system containing platform gyros and pendulous gyro
Algorithms were developed that attempt to identify which sensor in a tetrad configuration has experi...
Radio/optical/strapdown inertial guidance systems for unmanned interplanetary fligh
Flight test results of the strapdown inertial reference unit (SIRU) navigation system are presented....
Results of flight tests of the Strapdown Inertial Reference Unit (SIRU) navigation system are presen...
The theory, development, and test evaluations of the Strapdown Inertial Reference Unit (SIRU) are di...
The development and initial evaluation of a strapdown inertial reference unit (SIRU) system are disc...
The design, operation, performance and test of the gyro module and its circuit components are descri...
A complete description of the additional analysis, development and evaluation provided for the SIRU ...
The presence of failures in navigation sensors can cause the determination of an erroneous aircraft ...
The results of a study of test data taken on the simplex strapdown navigation system were presented....
Strapdown inertial measurement unit design, calculations, and operating instruction
A helicopter flight-test program to evaluate the performance of Honeywell's Tetrad - a strapdown, la...
The description, results, and interpretation is presented of comparison testing between the High Acc...
Motion-induced errors in strapdown inertial navigation systems are discussed. The errors generated i...
Proposed testing program for strapdown inertial system containing platform gyros and pendulous gyro
Algorithms were developed that attempt to identify which sensor in a tetrad configuration has experi...
Radio/optical/strapdown inertial guidance systems for unmanned interplanetary fligh
Flight test results of the strapdown inertial reference unit (SIRU) navigation system are presented....
Results of flight tests of the Strapdown Inertial Reference Unit (SIRU) navigation system are presen...
The theory, development, and test evaluations of the Strapdown Inertial Reference Unit (SIRU) are di...
The development and initial evaluation of a strapdown inertial reference unit (SIRU) system are disc...
The design, operation, performance and test of the gyro module and its circuit components are descri...
A complete description of the additional analysis, development and evaluation provided for the SIRU ...
The presence of failures in navigation sensors can cause the determination of an erroneous aircraft ...
The results of a study of test data taken on the simplex strapdown navigation system were presented....
Strapdown inertial measurement unit design, calculations, and operating instruction
A helicopter flight-test program to evaluate the performance of Honeywell's Tetrad - a strapdown, la...
The description, results, and interpretation is presented of comparison testing between the High Acc...
Motion-induced errors in strapdown inertial navigation systems are discussed. The errors generated i...
Proposed testing program for strapdown inertial system containing platform gyros and pendulous gyro
Algorithms were developed that attempt to identify which sensor in a tetrad configuration has experi...
Radio/optical/strapdown inertial guidance systems for unmanned interplanetary fligh