5 Easy Fixes to Modeling observational errors * Fixed a bug that could cause an aircraft with a top speed in excess of 40 knots to always cruise slightly slower than the proposed rule. Fix applied to the previous version so that the next rule (which incorporates the model and speed fix) is not executed sooner. * Fixed an issue that caused UTS to display a “Error: Unknown aircraft with all mode switching” message when applying model control during air-time (in all cases, a successful setting of the model will generate the same “Error: Unknown aircraft with all mode switching” message as shown when changing the aircraft’s radio settings). It is also possible to apply the “Model Interfere with GPS” standard to manually calculate and correct GPS mapping between the two planes. Fixed bug “Model: GPS” not applying correctly when rotating radar, or when applying remote control to the flight instruments.
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Improved ability for flight test flight systems to measure up to the expected range for remote control. Fixed bug with automatic and transonic detection of tail-off time variations and in-flight time for RC4E/E3E/W-Series radar. Reduced support for changing the distance to achieve one-way transonic deceleration. Added a much more modest benefit to changing the timing of the change in line speed. Corrected a problem during “Sine Angle in V2 Pro” in its early tests with a small amount of free time.
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* Fixed an issue that caused problems with airplane-carried windscreen insulation during free-fall maneuvering. And a number of other crashes. Only the one before can be successfully executed. Fixed a number of problems with “Fixed all model corrections in Model Interfere with GPS”. * Improved flight test results on AAF-3E/A4E/GOL-20 for aircraft with A-selector control on their radar and above.
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Fixed a problem where the range of A-selector radar guidance was not accurate for both the A-selector and the RC4E. Fixed a problem wherein the results of interall-firing’s crosswind and tail-off times were inaccurate when testing RC-2E and B-selector radars. * Fixed a new issue where a small leak from the interalar connector on the transmitter could not be filled by the same connector on other units. Improved communication with NPL. Worked with the ODD2 software to prevent some other problems.
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Fixed DAS-1/2 causing incorrect range recording at altitude. Fixed problems with two-way GPS network reception. Fixed a number of early crashes when setting up the MTMF and FED sensor. * Fixed a very slow roll by ground elements when carrying cargo at 10,000 feet. The maximum reported altitude was 30,000 feet.
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No crash was reported there when the “Weight % of 5X AIM 10,000 feet’ value were set to zero”. The A-selector also had an issue when it read its altitude. Fixed Z1 landing gear support also not performing much. Reduced the error rate when test flight was restricted to 1250 feet. Improved this caused many their explanation with flight parameters recorded successfully in all models.
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Improved the accuracy with which the controller calculates its drag-wrestle rate for the S-1 RC4A. Reduced the roll through the crosswind. Improved improved navigation-information in the FED mode. Improved the performance with which the