NASA Technical Reports Server (NTRS) 19770024181: A Description Of The Software Analysis From Flight And Simulation Data Of The Course Cut Limiter In The TCV B-737 Area Navigation Computer - Info and Reading Options
By NASA Technical Reports Server (NTRS)
"NASA Technical Reports Server (NTRS) 19770024181: A Description Of The Software Analysis From Flight And Simulation Data Of The Course Cut Limiter In The TCV B-737 Area Navigation Computer" and the language of the book is English.
“NASA Technical Reports Server (NTRS) 19770024181: A Description Of The Software Analysis From Flight And Simulation Data Of The Course Cut Limiter In The TCV B-737 Area Navigation Computer” Metadata:
- Title: ➤ NASA Technical Reports Server (NTRS) 19770024181: A Description Of The Software Analysis From Flight And Simulation Data Of The Course Cut Limiter In The TCV B-737 Area Navigation Computer
- Author: ➤ NASA Technical Reports Server (NTRS)
- Language: English
Edition Identifiers:
- Internet Archive ID: NASA_NTRS_Archive_19770024181
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"NASA Technical Reports Server (NTRS) 19770024181: A Description Of The Software Analysis From Flight And Simulation Data Of The Course Cut Limiter In The TCV B-737 Area Navigation Computer" Description:
The Internet Archive:
During automatic horizontal path captures, the (Terminal Configured Vehicle) B-737 airplane maintained smaller than designed path intercept angles and experienced a sawtooth bank angle oscillation during its turn towards the path. From flight data, it was determined that these anomalies were caused by the improper output of the course cut limiter in the horizontal path control law. The output from the course cut limiter did not obtain its full value and it was calculated stepwise discontinuously. The automatic horizontal path captures were then conducted on the TCV B-737 airplane real-time simulation. The path intercept angles were maintained properly and no bank angle oscillation was encountered. Data showed that the course cut limiter was calculated at its full value in a continuous manner. The intermediate calculations of the course cut limiter in the airplane's navigation computer were rewritten and rescaled in such a manner that truncation errors could be minimized. The horizontal path capture tests were then reflown. The airplane maintained the proper path intercept angle and no bank angle oscillations occurred on any of the tests.
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