An overview of the design and development of lunar rover (Chandrayaan-2) for space applications
AUTHOR(S)
Lohit Nimbagal, Rahul M., Sneha N. Teggi, Sushmitha M.R., Dr. Pavithra G., Dr. Sindhu Shree M., Dr. T.C.Manjunath, Aditya T.G., Sandeep K.V., Rajashekar M. Koyyeda,Dr. Suhasini V.K., Dr. Vijayakumar K.N.
DOI: https://doi.org/10.46647/ijetms.2023.v07i01.032
ABSTRACT
The paper gives an brief overview of the design and development of lunar rover (Chandrayaan-2) for space applications. The Moon has always been the center of attention for mankind, more than any other heavenly body in More than any other heavenly body in the night sky, the Moon has long been the focus of human interest. The Moon has always presented mankind with a challenge to learn more about it and to marvel at its wonders because it bears the early history of the solar system. We can uncover the early evolution of the solar system and that of planet Earth by having a better understanding of the Moon. With the 2008 launch of the Chandrayaan-1 orbiter mission to the Moon, India's planetary exploration program was launched by the Indian Space Research Organization (ISRO). India launched Chandrayaan-2, its second lunar exploration mission, nearly twelve years after its first lunar exploration mission. Chandrayaan-2, India's most technologically advanced aircraft, is on an unprecedented mission. The South Polar Region of the Moon will be studied by India's second lunar trip, which will draw on nearly ten years of scientific and Engineering advancement. A major accomplishment for both India and humanity, Chandrayaan-2 was the first mission ever to be sent to the southern pole of the moon. Both the high cold and constant darkness in this area make it extremely unsafe and have a bad impact on missions. India faced a tremendously difficult assignment as a result, and the entire world was interested in its outcome. Chandrayaan-1's eleven remote-sensing scientific instruments from ISRO, NASA, and ESA have made important discoveries, such as the identification of a water signature, the discovery of spinel minerals, lunar lava tubes, signs of recent volcanism, impact-triggered boulder movements, and the detection of sputtered atomic oxygen and backscattered helium on the lunar surface. Three components made up Chadrayaan-2: an orbiter, a lander, and a rover. 2019 saw the launch of this mission. During this mission, the Orbiter was successful in reaching the moon's orbit, but communication with the Lander was lost, which caused Lander to perform poorly and crash with the Pragyan rover and other scientific equipment. The work given here is a mini-project that is taken up as a part of the curriculum completed by electronics and communication engineering students in the second year of the electronics & communication engineering department at Dayananda Sagar College of Engineering in Bangalore.
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References:
- Duda, Kevin R., Michael C. Johnson, and Thomas J. Fill., “Design and analysis of lunar lander manual control modes”, 2009 IEEE Aerospace conference, pp. 1-16, IEEE, 2009.
- Acharya, Hardik, T. P. Srinivasan, and B. GopalaKrishna, “A new approach for terrain analysis of lunar surface by Chandrayaan-1 data using open source libraries”, 2013 Fourth National Conference on Computer Vision, Pattern Recognition, Image Processing and Graphics (NCVPRIPG), pp. 1-4. IEEE, 2013.
- Aneesh, R.P., Dinakar Prasad Vajja, P. P. Pramod, PS Ajeesh Kumar, and Arun Peethambaran, “Spacecraft command and data system simulator for the payload chaste in Chandrayaan-2 mission”, 2017 IEEE International Conference on Circuits and Systems (ICCS), pp. 97-102. IEEE, 2017.
- Calla, O. P. N., Shubhra Mathur, and Kishan Lal Gadri, “Possible Landing site for Chandrayaan-2 Rover”, 2016 International Conference on Recent Advances and Innovations in Engineering (ICRAIE), pp. 1-5. IEEE, 2016.
- Wan, Junlin, Hong Nie, Jinbao Chen, and Qing Lin, “Modeling and simulation of Lunar lander soft-landing using transient dynamics approach”, 2010 International Conference on Computational and Information Sciences, pp. 741-744. IEEE, 2010.
- Rui, Xu, Jiang Huiping, Tang Shengjing, Cui Pingyuan, and Yue Fuzhan, “Analyzing and designing of lunar rover motion controller”, 2007 IEEE International Conference on Robotics and Biomimetics (ROBIO), pp. 1574-1579. IEEE, 2007.
- Harrison, Dan A., Robert Ambrose, Bill Bluethmann, and Lucien Junkin, “Next generation rover for lunar exploration”, 2008 IEEE aerospace conference, pp. 1-14. IEEE, 2008.
- Mark Williamson, “Analysis asian moon - Briefing in depth”, IEEE- Engineering & Technology, vol. 3, no. 21, pp. 6-19, December 2008.
- Charles D. Brown, “Elements of spacecraft design”, AIAA, 2002.
- Mehran Sarkarati and Mariella Spada, “Developing operational spacecraft simulators”, Proceedings of the DASIA 2008- Data systems in Aerospace.
- Arnold Hanslmeier, “The Sun and Space Weather”, Springer.
- James Joseph, “Papike text book Planetary Materials”, Mineralogical Society of America, 1998.
- Dinakar Prasad Vajja, PP Pramod and PS Ajeeshkumar, “Design Document of Processing Electronics of ChaSTE Payload on Chandrayaan-2 Lander”, TR-SPL-CH2-ChaSTE-PE, 2015.
- A.H.G. AL-DHAHER, “Development of Microcontroller/FPGA-based systemsInt”, J. Engng, vol. 20, no. 1, pp. 52-60, 2004.
- MESA-introduction document round table conference on 2010 , European Space Agency.
- E. Marsch, H.-J. Fahr and K., text book: The Outer Heliosphere: The Next Frontiers.
- Dinakar Prasad Vajja, PP Pramod and PS Ajeeshkumar, “Electrical Interconnection Details (EID) of ChaSTE Payload on Chandrayaan-2 Lander”, TR-SPL-CH2-ChaSTE-EID, 2015.
- R. Devi Priya, R. Sivaraj, Ajith Abraham, T. Pravin, P. Sivasankar and N. Anitha. "Multi-Objective Particle Swarm Optimization Based Preprocessing of Multi-Class Extremely Imbalanced Datasets". International Journal of Uncertainty, Fuzziness and Knowledge-Based Systems Vol. 30, No. 05, pp. 735-755 (2022). Doi: 10.1142/S0218488522500209
- Dinakar Prasad Vajja, PP Pramod and PS Ajeeshkumar, “Interface Document for Processing Electronics and Frontend Electronics of ChaSTE Payload on Chandrayaan-2 Lander”, TR-SPL-CH2-ChaSTE-ID, 2015.
- Chirag H B; Darshan M; Rakesh M D; Priyanka D S; Manjunath Aradya. "Prediction of Concrete Compressive Strength Using Artificial Neural Network". International Research Journal on Advanced Science Hub, 4, 11, 2022, 281-287. doi: 10.47392/irjash.2022.069
- PP Pramod, PS Ajeeshkumar, Vajja Dinakar Prasad and Vijaykumar S Nair, "Design and Development of Data Disseminator for BC Measurements for Remote ARFI Observatories", ISRO-VSS C-TR-0523–0-15, 2015.
- Honey Well, Temperature sensors HEL-700 Series Platinum RTD datasheet.
How to Cite This Article:
Lohit Nimbagal, Rahul M., Sneha N. Teggi, Sushmitha M.R., Dr. Pavithra G., Dr. Sindhu Shree M., Dr. T.C.Manjunath, Aditya T.G., Sandeep K.V., Rajashekar M. Koyyeda,Dr. Suhasini V.K., Dr. Vijayakumar K.N.
. An overview of the design and development of lunar rover (Chandrayaan-2) for space applications . ijetms;7(1):232-236. DOI: 10.46647/ijetms.2023.v07i01.032