AEROSPACE SYSTEMS provides an international, peer-reviewed forum which focuses on system-level research and development regarding aeronautics and astronautics. The journal emphasizes the unique role and increasing importance of informatics on aerospace. It fills a gap in current publishing coverage from outer space vehicles to atmospheric vehicles by highlighting interdisciplinary science, technology and engineering. Potential topics include, but are not limited to: - Trans-space vehicle systems design and integration - Air vehicle systems - Space vehicle systems - Near-space vehicle systems - Aerospace robotics and unmanned system - Communication, navigation and surveillance - Aerodynamics and aircraft design - Dynamics and control - Aerospace propulsion - Avionics system - Opto-electronic system - Air traffic management - Earth observation - Deep space exploration - Bionic micro-aircraft/spacecraft - Intelligent sensing and Information fusion
Aerospace Systems
Description
Identifiers
ISSN | 2523-3947 |
e-ISSN | 2523-3955 |
Publisher
Springer Singapore
Additional information
Data set: Springer
Articles
Aerospace Systems > 2019 > 2 > 2 > 83-95
Angular velocity plays a critical role in determining the outcome of a close-range aerial engagement between two identical fighter aircraft pitching at full deflection. In a zero gravity environment, a pursuer may exploit its ability to roll to increase its relative angular velocity against a pitching opponent. In this paper, we present a repeatable maneuver for an unmanned fighter aircraft that increases...
Aerospace Systems > 2019 > 2 > 2 > 97-104
Microelectromechanical systems’ (MEMS) inertial measurement unit (IMU) is widely used in many scenarios for its small size, low weight, and low-power consumptions. However, it possesses relatively low positioning accuracy compared with other high-grade IMUs, as errors accumulate quickly over time. This paper mainly focuses on the error characteristics of the gyro part of MEMS IMU by analyzing different...
Aerospace Systems > 2019 > 2 > 2 > 155-161
The manuscript discusses issues related to the use of mathematical modeling to substantiate the reliability and safety of the Superjet-100 aircraft during the emergency landing. The problem of the passenger airplane airframe dynamic deformation in the landing with partially removed and released the landing gear under given initial conditions of touching the runway of the airfield. Confirmation of...