Results 61 to 70 of about 899,057 (211)

Loran-C flight test software [PDF]

The software package developed for the KIM-1 Micro-System and the Mini-L PLL receiver to simplify taking flight test data is described along with the address and data bus buffers used in the KIM-1 Micro-system.
Nickum, J. D.
core   +1 more source

INFORMATION SECURITY IN MOBILE MODULAR MEASURING SYSTEMS

Научный вестник МГТУ ГА, 2018
A special aspect of aircraft test is carrying out both flight evaluation and ground operation evaluation in a structure of flying aids and special tools equipment. The specific of flight and sea tests involve metering in offshore zone, which excludes the
A. N. Tkhishev, P. S. Gorshkov, A. P. Golovkin   +2 more
doaj   +1 more source

Executable assertions and flight software [PDF]

Executable assertions are used to test flight control software. The techniques used for testing flight software; however, are different from the techniques used to test other kinds of software.
Andrews, D. M., Mahmood, A., Mccluskey, E. J.   +2 more
core   +1 more source

Analytical testing [PDF]

Analytical methods for combining flight acceleration and strain data with shake test mobility data to predict the effects of structural changes on flight vibrations and strains are presented.
Fabunmi, J. A., Flannelly, W. G., Nagy, E. J.   +2 more
core   +1 more source

Aerodynamic investigation by experimental and computational simulation of a flying wing unmanned aerial vehicle for cargo delivery and surveillance missions

Aviation
Baseline-IX is a tailless aircraft design with compound wing attached to a short body, a transition between a straight, swept flying wing design and a blended wing-body.
Atikah Basyirah Abdul Muta’ali, Rizal Effendy Mohd Nasir, Wahyu Kuntjoro   +2 more
doaj   +1 more source

Numerical and flight simulator test of the flight deterioration concept [PDF]

Manned flight simulator response to theoretical wind shear profiles was studied in an effort to calibrate fixed-stick and pilot-in-the-loop numerical models of jet transport aircraft on approach to landing.
Mccarthy, J., Norviel, V.
core   +1 more source

Orbiter emergency crew escape system [PDF]

, 1980
Two conventional ejection seats were incorporated into the first two orbiter vehicles to provide the crew with emergency ejection capability during the flight test programs.
Lofland, W. W.
core   +1 more source

An Underwater Multisensor Fusion Simultaneous Localization and Mapping System Based on Image Enhancement

Journal of Marine Science and Engineering
As a key method of ocean exploration, the positioning accuracy of autonomous underwater vehicles (AUVs) directly influences the success of subsequent missions.
Zeyang Liang, Kai Wang, Jiaqi Zhang, Fubin Zhang   +3 more
doaj   +1 more source

Navigation and flight director guidance for the NASA/FAA helicopter MLS curved approach flight test program [PDF]

The navigation and flight director guidance systems implemented in the NASA/FAA helicopter microwave landing system (MLS) curved approach flight test program is described. Flight test were conducted at the U.S.
Lee, M. G., Phatak, A. V.
core   +1 more source

A LTA flight research vehicle [PDF]

, 1975
An Airship Flight Research Program is proposed. Major program objectives are summarized and a Modernized Navy ZPG3W Airship recommended as the flight test vehicle. The origin of the current interest in modern airship vehicles is briefly discussed and the
Nebiker, F. R.
core   +1 more source