Advances in Small Satellite Technologies

Proceedings of 1st International Conference on Small Satellites
1. Auflage 2020
ISBN: 978-981-15-1723-5
Verlag: Springer Nature Singapore

Buch, Englisch, 544 Seiten, Format (B × H): 160 mm x 241 mm, Gewicht: 1100 g

Reihe: Lecture Notes in Mechanical Engineering

This volume contains select papers presented during the 1st International Conference on Small Satellites, discussing the latest research and developments relating to small satellite technology. The papers cover various issues relating to design and engineering, ranging from the control, mechanical and thermal systems to the sensors, antennas and RF systems used. The volume will be of interest to scientists and engineers working on or utilizing satellite and space technologies.

Zielgruppe

Research

Autoren/Hrsg.

Sastry, Psr Srinivasa

Rao, Samba Siva

CV, Jiji

Raghavamurthy, D. V. A.

Fachgebiete

• Technische Wissenschaften Verkehrstechnik | Transportgewerbe Luft- und Raumfahrttechnik, Luftverkehr
• Mathematik | Informatik EDV | Informatik Informatik Künstliche Intelligenz
• Technische Wissenschaften Technik Allgemein Mess- und Automatisierungstechnik
• Naturwissenschaften Physik Angewandte Physik Astrophysik
• Naturwissenschaften Astronomie Astrophysik

Inhaltsverzeichnis

Channels Multi-Sensors Interface CMOS IC for Telemetry Application.- Study of concurrent piezo actuation and sensing on drift stability of CVGs.- A quantitative comparator of heuristic methods for optimal route in hilly terrain.- Simulation of the Dynamics and Control of Tethered Small Satellite Deployment.- Design and development of mass optimised Isolation Latch Valve for Chandrayaan 2 Lander Propulsion.- De-Tumbling Controller of NIUSAT.- The Configurable Attitude Control System(ACS) Test System Design for RSAT Test System.- Optimal Nonlinear Dynamic Inversion Based Flight Control System Design for an Aerospace Vehicle.- Closed Loop Simulation for Attitude Control of Nano-satellite.- Real-Time Autonomous Navigation Scheme for Pointing.- Mission and control configuration for spin to 3-axis stabilization for small satellite.

Über Autor(innen)

PSR Srinivasa Sastry is the Project Director for the first LEO Satellite of Defence Research and Development Organization. In RCI he has worked for the development of hydraulic and electo-mechanical actuation systems for AGNI, A1 to A5 and Interceptor Missiles AD, and designed and developed several electro-hydraulic and electro-mechanical actuators, analog and digital controllers

Jiji CV is a Professor in the Department of Electronics and Communication, College of Engineering Trivandrum (CET), where his research focuses on computer vision, image processing, computational photography and signal processing.He has done his M. Tech and PhD from Indian Institute of Technology Bombay. He is also a visiting researcher in the University of Trento, Italy.

D.V.A Raghavamurthy is a the Director of Aerospace Research in Veltech University. He joined ISRO as a Systems Engineer after his M.Sc.(Tech) from REC Warangal, and worked on numerous satellite projects, including Bhaskara-II, TES, and IRS satellites. He was Project Director of Cartosat-1, IMS-1, YouthSat, SARAL and first Project Director of Chandrayaan 2. He had also been involved in small satellite projects till 2013, when he became the Director of the Earth Observations System in ISRO Head Quarters and was responsible for Earth observing satellites, missions and applications till his retirement in 2016.

V. Sambasiva Rao is a Professor in the Electrical and Communications Engineering Department in PES University and the Director of the Crucible of Research & Innovation (CORI), Bangalore. An engineering graduate from College of Engineering, Kakinada, (Andhra University), he obtained his Ph.D from BITS, Pilani, and was associated with ISRO in various capacities for 37 years, till his retirement as Deputy Director from ISRO Satellite Centre in June 2011. In ISROhe was responsible for the development of high bit rate data transmitters for all IRS series of satellites and various RF and microwave systems in S, C, X, Ku and Ka bands for IRS and INSAT missions, and was also associated with the planning of communication satellites and development of associated technologies.