Actuation System Simulation and Validation in Hardware in Loop Simulation (HILS) for an Aerospace Vehicle
Actuation System Simulation and Validation in Hardware in Loop Simulation (HILS) for an Aerospace Vehicle
- New search for: Prasad, M. V. K. S.
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- New search for: Satapathy, Suresh Chandra
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- New search for: Favorskaya, Margarita N.
- New search for: Prasad, M. V. K. S.
- New search for: Patri, Sreehari Rao
- New search for: Nayak, Jagannath
An Aerospace vehicle is developed as a result of integration of many subsystems with each subsystem marked to perform a particular function. The heart of the Aerospace vehicle is the control and guidance computer known as On-board computer. The rate gyroscopes which sense the aerospace vehicle rates and the accelerometers which sense accelerations are embedded in sensor system package. The Actuation system of the aerospace vehicle helps in steering the vehicle to the required direction. The Aerospace vehicle’s guidance algorithm calculates the correction required to move the vehicle to the intended trajectory. This error is converted into control deflection commands by the Autopilot. These deflection commands are given to the hardware actuation system so that the vehicle course is changed as per design. In this paper simulation of actuator model and Hardware-In-Loop-Simulation (HILS) of hardware actuation system is presented.
Document information
Actuation System Simulation and Validation in Hardware in Loop Simulation (HILS) for an Aerospace Vehicle
Learning and Analytics in Intelligent Systems
International Conference on E-Business and Telecommunications ; 2019 ; Hyderabad, India March 22, 2019 - March 23, 2019
Advances in Decision Sciences, Image Processing, Security and Computer Vision ; Chapter : 23 ; 194-200
2019-07-26
7 pages
Article/Chapter (Book)
Electronic Resource
English
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