Table of contents
Fault detection of reaction wheels in attitude control subsystem of formation flying satellites: A dynamic neural network-based approach
Shima Mousavi, Khashayar KhorasaniA decentralized dynamic neural network (DNN)-based fault detection (FD) system for the reaction wheels of satellites in a formation flying mission is proposed. The paper aims to…
404
Three biomimetic flight control sensors
Javaan ChahlInsects depend on the spatial, temporal and spectral distribution of light in the environment for navigation, collision avoidance and flight control. The principles of insect…
529
Verification of a special inertial measurement unit using a Quadrotor aircraft
Angel Flores-Abad, Pu Xie, Gabriela Martinez-Arredondo, Ou Ma– Calibration and 6-DOF test of a unique inertial measurement unit (IMU) using a Quadrotor aircraft. The purpose of this paper is to discuss the above issue.
279
ISSN:
2049-6427Online date, start – end:
2013Copyright Holder:
Emerald Publishing LimitedOpen Access:
hybridEditor:
- Mr John Page