• Journals

  1. J. V. Pushpangathan, K. Harikumar, S. Sundaram, and N. Sundararajan, ``Robust Simultaneously Stabilizing Decoupling Output Feedback Controllers for Unstable Adversely Coupled Nano Air Vehicles," IEEE Trans. Syst., Man, Cybern., Syst., early access, Sept. 13, 2020, DOI: 10.1109/TSMC.2020.3. Paper Link

  2. J. V. Pushpangathan, Harikumar, K., and Bhat, M. S., ``v-gap Metric Based Simultaneous Frequency-Shaping Stabilization for Unstable Multi-Input Multi-Output Plants", Journal of Guidance, Control, and Dynamics, Vol. 41, No. 12, Dec. 2018. Paper Link

  3. J. V. Pushpangathan, Bhat, M. S., and Harikumar, K., ``Effects of Gyroscopic Coupling and Countertorque in a Fixed-Wing Nano Air Vehicle,'' Journal of Aircraft, Vol. 55, No. 1, Jan.-Feb. 2018, pp. 239-250. Paper Link

  4. J. V. Pushpangathan, Harikumar, K., and Bhat, M. S., ``75 mm Wingspan Fixed-Wing Nano Air Vehicle with a Novel Aircraft Configuration,'' IEEE ACCESS, Vol. 6, pp. 74521-74535, Nov. 2018. Paper Link

  5. J. V. Pushpangathan, Kandath H., and Balakrishnan A., ``Hit-to-kill Accurate Minimum Time Continuous Second-Order Sliding Mode Guidance for Worst-Case Target Maneuvers", Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, Sept. 2020. DOI:10.1177/0954410020954977.Paper Link

  6. J. V. Pushpangathan, Srinivasan, K., and Bhat, M. S., ``Design and Development of Fixed-Wing Nano Air Vehicle,'' Journal of Unmanned System Technology, Vol. 2, May 2014, pp. 30-39. Paper Link

  7. Kandath H., J. V. Pushpangathan, and Sundaram S., ``Effects of Propeller Flow on the Longitudinal and Lateral Dynamics and Model Couplings of a Fixed-Wing Micro Air Vehicle", Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, Oct. 2020. October 2020. DOI:10.1177/0954410020966155.Paper Link

  8. Kandath H., J. V. Pushpangathan, Dhall S., and Bhat M. S., ``Integrated Guidance and Control Framework for the Waypoint Navigation of a Miniature Aircraft with Highly Coupled Longitudinal and Lateral Dynamics", Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, Oct. 2020. Oct. 2020. October 2020. DOI:10.1177/0954410020964992.Paper Link

  9. Kandath, H., J. V. Pushpangathan, Bera, T., Dhall, S., and Bhat, M. S., ``Modeling and Closed Loop Flight Testing of a Fixed Wing Micro Air Vehicle,'' Micromachines, Vol. 9, No. 3, Article No. 111, 4 Mar. 2018. Doi:10.3390/mi9030111. Paper Link

  • Conferences

  1. J. V. Pushpangathan, Karthik, S., and Bhat, M. S., ``Design and Development of Fixed Wing Nano Air Vehicle," Proceedings of 9th International Conference on Intelligent Unmanned Systems, Jaipur, Rajasthan, India, ICIUS-2013- 174, Sep. 2013.

  2. J. V. Pushpangathan, ``Second-order Sliding Mode Based Guidance Law for Missile Interceptor,'' Proceedings of 1st International conference on Technological Trends (ICTT 2010), Trivandrum, Kerala, India, 2010.

  3. J. V. Pushpangathan, and Ajithkumar, B., ``Higher-order Optimal Sliding Mode Guidance for Interceptor Missile,'' Proceedings of 12th National conference on Technological Trends (NCTT 2011), Trivandrum, Kerala, India, 2011.

  • Technical Reports

  1. M. Seetharama Bhat, S.N. Omkar, K. Harikumar, Jinraj V. Pushpangathan, T. Bera, S. Karthik, S. Dhall and A. Eobin , ``Development of Autonomous Robust Fixed Wing Micro Air Vehicle", Department of Aerospace Engineering, Indian Institute of Science, Bangalore, Technical Report No: AE/MSB/DRDO-NPMICAV-TR-2013-002, Oct. 2013.

  2. M. Seetharama Bhat, S.N. Omkar, K. Harikumar, Jinraj V. Pushpangathan, T. Bera, S. Karthik, S. Dhall and Pradyumna M K , ``Development of Autonomous Robust Fixed Wing Micro Air Vehicle", Department of Aerospace Engineering, Indian Institute of Science, Bangalore, Technical Report No: AE/MSB/DRDO-NPMICAV-TR-2013-003, Dec. 2013.

  3. M. Seetharama Bhat, S.N. Omkar, K. Harikumar, T. Bera, Jinraj V. Pushpangathan, S. Jana,S.Dhall and Akhil Thomas, ``Development of Autonomous Robust Fixed Wing Micro Air Vehicle", Department of Aerospace Engineering, Indian Institute of Science, Bangalore, Technical Repor No: AE/MSB/DRDO-NPMICAV-TR-2014-001, Sep. 2014.

  4. M. Seetharama Bhat, and Jinraj V. Pushpangathan, ``Design and Development of 75~mm Fixed-wing Nano Air Vehicle", Department of Aerospace Engineering, Indian Institute of Science, Bangalore, Technical Repor No: AE/MSB/DRDO-NPMICAV-TR-2016-006, April 2016.