Results 121 to 130 of about 32,114 (240)

Software for strapdown inertial navigation system.

Journal of the Japan Society for Aeronautical and Space Sciences, 1988
Kenichiro KATAOKA, Hirofumi EGUCHI
openaire   +2 more sources

Initial specifications for van and aircraft [PDF]

Proposed testing program for strapdown inertial system containing platform gyros and pendulous ...
Benson, D. O., Jr., Fincke, W. H.
core   +1 more source

Inertial gyroscope system application considerations [PDF]

Criteria for designing inertial gyroscope ...
Booth, R. A., Harlow, R. R.
core   +1 more source

Centaur D-1A guidance/software system [PDF]

The main body of this paper describes the evolution of the Centaur D-1A Guidance and Software System. Specifically, the performance of the explicit guidance equations, using a linear tangent steering law.
Gordan, A. L.
core   +1 more source

Operational alignment and calibration of the ISU for phase 2 of the V/STOL program. Volume 2 - Alignment [PDF]

Strapdown inertia system for V/STOL program with theoretical error analysis using Kalman filter estimation theory and computer ...
Benson, D. O., Jr., Rome, H. J.
core   +1 more source

Fast Compass Alignment for Strapdown Inertial Navigation System

Computers, Materials & Continua, 2020
Jin Sun, Dengyin Zhang, Xiaoye Shi, Fei Ding   +3 more
openaire   +1 more source

Estimation and filtering techniques for strapdown inertial navigators

, 1980
Imperial Users ...
Wright, G. C., Wright, G. C.
openaire   +1 more source

Uranium dioxide fuel cladding strain investigation with the use of CYGRO-2 computer program [PDF]

Previously irradiated UO2 thermionic fuel pins in which gross fuel-cladding strain occurred were modeled with the use of a computer program to define controlling parameters which may contribute to cladding strain.
Smith, J. R.
core   +1 more source

Effectiveness evaluation of STOL transport operations (phase 2) [PDF]

A computer simulation program which models a commercial short-haul aircraft operating in the civil air system was developed. The purpose of the program is to evaluate the effect of a given aircraft avionics capability on the ability of the aircraft to ...
Brown, R. A., Kuhner, M. B., Ullman, D. G., Welp, D. W.   +3 more
core   +1 more source

Theoretical error modeling and analysis of strapdown inertial navigation system alignment under zero-velocity conditions. [PDF]

Sci Rep
Mohammadkarimi H, Mobtaker M, Alizadeh MH.   +2 more
europepmc   +1 more source