Inertial sensor arrays—A literature review
JO Nilsson, I Skog - 2016 European Navigation Conference …, 2016 - ieeexplore.ieee.org
Inertial sensor arrays present the possibility of improved and extended sensing capabilities
as compared to customary inertial sensor setups. Inertial sensor arrays have been studied …
as compared to customary inertial sensor setups. Inertial sensor arrays have been studied …
Innovative photonic sensors for safety and security, part II: aerospace and submarine applications
The employability of photonics technology in the modern era's highly demanding and
sophisticated domain of aerospace and submarines has been an appealing challenge for …
sophisticated domain of aerospace and submarines has been an appealing challenge for …
Load monitoring of aircraft landing gears using fiber optic sensors
A Iele, M Leone, M Consales, GV Persiano… - Sensors and Actuators A …, 2018 - Elsevier
We report on the use of Fiber Bragg Grating (FBG) sensors integrated onto an aircraft
landing gear for remote and real-time load monitoring. Several FBGs strain sensors, both in …
landing gear for remote and real-time load monitoring. Several FBGs strain sensors, both in …
Attitude measurement for high-spinning projectile with a hollow MEMS IMU consisting of multiple accelerometers and gyros
F Liu, Z Su, H Zhao, Q Li, C Li - Sensors, 2019 - mdpi.com
A low cost, high precision hollow structure MEMS IMU has been developed to measure the
roll angular rate of a high-spinning projectile. The hollow MEMS IMU is realized by …
roll angular rate of a high-spinning projectile. The hollow MEMS IMU is realized by …
Snake aerial manipulators: A review
J Mendoza-Mendoza, VJ Gonzalez-Villela… - IEEE …, 2020 - ieeexplore.ieee.org
In this document, a review about snake aerial manipulators is presented. The most common
mechatronical implications found in their design are described. The text is presented to the …
mechatronical implications found in their design are described. The text is presented to the …
Management and intelligent control of in‐flight fuel distribution in a commercial aircraft
E Plaza, M Santos - Expert Systems, 2024 - Wiley Online Library
Fuel management is an important issue in aviation for safety and efficiency reasons. This
work develops an alternative solution based on an artificial intelligent technique to the fuel …
work develops an alternative solution based on an artificial intelligent technique to the fuel …
An analytical modelling of demand for driving torque of a wheelchair with electromechanical drive
This study aimed at analysing the influence of the position of the centre of gravity variability
and the movement velocity on the demand for a torque and work time coverage of a …
and the movement velocity on the demand for a torque and work time coverage of a …
Gyro-free inertial measurement unit with unfettered accelerometer array distribution and for the object with position change in center of gravity
P Yang, Y Chen, Y Chen, F Dang - IEEE Sensors Journal, 2021 - ieeexplore.ieee.org
Previous gyro-free inertial measurement units (GF-IMU) usually suffered from installation
errors induced by mutual placements and mutual sensing directions of accelerometers, and …
errors induced by mutual placements and mutual sensing directions of accelerometers, and …
A multi-scaled demonstrator for aircraft weight and balance measurements based on FBG sensors: Design rationale and experimental characterization
Abstract A multi-scaled W&B demonstrator able of reproducing the same loading condition
of an aircraft as a whole is designed, manufactured and experimentally characterized. Two …
of an aircraft as a whole is designed, manufactured and experimentally characterized. Two …
[HTML][HTML] Sensitivity analysis and flight tests results for a vertical cold launch missile system
R Głębocki, M Jacewicz - Aerospace, 2020 - mdpi.com
In vertical cold launch the missile starts without the function of the main engine. Over the
launcher, the attitude of the missile is controlled by a set of lateral thrusters. However, a …
launcher, the attitude of the missile is controlled by a set of lateral thrusters. However, a …