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Adiga, BS and Muralidhar, SJ and Nagabhushana, S and Viswanathan, R (1991) Techniques for analysis of cockpit voice recorder. Project Report. National Aerospace Laboratories, Bangalore.
Adiga, BS and Murthy, NN (1986) Aircraft parameter estimation, control and simulation (APECS) computer: Evaluation of final offers. Project Report. National Aerospace Laboratories, Bangalore.
Ailneni, S and Kashyap, SK and Naidu, VPS and Kumar, A (2021) Angle only Tracking for Infrared Search and Track (IRST) System Mounted on an Aircraft. In: 2021 7th Indian Control Conference, December 20-22, 2021, Mumbai.
Ailneni, S and Kashyap, SK and Shantha Kumar, N and David Livingstone, D and Aishwarya, N and Varghese, N and Karthik, KV (2019) Characterization of MEMS based Inertial Measurement Unit. In: 2019 International Conference on Range Technology (ICORT), 15-17 Feb, 2019, Balasore, India.
Amit, Khatri and Jatinder, Singh and Nandan, Sinha (2014) Aircraft Design Using Constrained Bifurcation and Continuation Method. Journal of Aircraft, 51 (5). pp. 1647-1652. ISSN 0021-8669
Amit, Khatri and Jatinder, Singh and Nandan, Sinha (2013) Aircraft Design Using Constrained Bifurcation and Continuation Method. In: AIAA Atmospheric Flight Mechanics (AFM) Conference, August 19-22, 2013, Boston, Massachusetts.
Ananda, CM (2007) Civil Aircraft Advanced Avionics Architecutres - An Insight Into Saras Avionics, Present and Future Perspective13;. In: Symposium on Aircraft Design, 14th June 2007, Bangalore, India.
Anju, Sharma (2021) Development of LabVIEW based mass flow plug control for wind tunnel application. In: AIP Conference Proceedings 2316.
Ashok, G and Karthik, K and Sathish, BG and Rohidekar, R Satish (1991) Nalla 1 : Data report-Part I. Technical Report. National Aerospace Laboratories, Bangalore, India.
Augustin, M.J and Ramesh, V and Prasad, RK and Gupta, N and Kumar, MR (2021) Detection of inclusion by using 3D laser scanner in composite prepreg manufacturing technique using convolutional neural networks. Machine Vision and Applications, 32 (6). ISSN 09328092
Babu, AVS and Pradeepa, S and Siva Subba Rao, P (2015) Closed loop control system based hybrid energy system model. In: 6th International Conference on Advances in Computing, Control, and Telecommunication Technologies, ACT 2015, 2015.
Babu, MD and Prabhakar, G and Jeevithashree, DV and Saluja, KPS and Pashilkar, AA and Biswas, P (2019) Using Eye gaze tracker to automatically estimate pilots' cognitive load. In: 50th Annual International Symposium of the Society of Flight Test Engineers.
Balakrishna, S and Niranjana, T (1986) Moment Stability Derivatives of Prithvi Missile Configuration at Low Speed Using Semi Free Dynamic Flying Method -Proposal. Project Report. National Aerospace Laboratories, Bangalore.
Balakrishna, S and Niranjana, T and Rajan, SR (1991) Augmentation of the 1.2m x 1.2m low speed dynamic test wind tunnel at NAL. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Balakrishna, S and Niranjana, T and Rajan, SR (1992) A rotary derivative rig for FMCD low speed tunnel. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Basappa, K (2004) Evaluation of Recursive Methods for Aircraft Parameter Estimation. In: AIAA Atmospheric Flight Mechanics Conference and Exhibit, 16-19 August 2004,, Providence, Rhode Island.
Biswas, K. (2018) Military airworthiness and certification procedures: Global scenario. Lecture Notes in Mechanical Engineering. pp. 315-331. ISSN 21954356
Chandrasekaran, K and Theningaledathil, V and Hebbar, A (2021) Ground based variable stability flight simulator. Aviation, 25 (1). pp. 22-34. ISSN 16487788
Chetty, Shyam (1988) Design of robust flight control systems. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Datta, A and Augustin, MJ and Gupta, N and Viswamurthy, SR and Gaddikeri, KM and Sundaram, R (2021) Strain sensor's network for low-velocity impact location estimation on carbon reinforced fiber plastic structures: Part-II. Indian Journal of Pure and Applied Physics, 59 (10). pp. 678-686.
Datta, A and Augustin, MJ and Gupta, Nitesh and Viswamurthy, SR and Gaddikeri, KM and Sundaram, Ramesh (2019) Impact Localization and Severity Estimation on Composite Structure Using Fiber Bragg Grating Sensors by Least Square Support Vector Regression. IEEE Sensors Journal, 19 (12). pp. 4463-4470. ISSN 1530437X
Deshpande, P J and Modani, A (2019) Experimental investigation of fluid–structure interaction in a bird-like flapping wing. Journal of Fluids and Structures, 91. ISSN 08899746
Dhanalakshmi, K and Mathur, JS and Chakrabartty, SK (2003) Radomes for JAGUAR aircraft: Closure Report. Technical Report. National Aerospace Laboratories, Bangalore.
George, SM and Selvi, SS and Raol, JR (2022) Aircraft Parameter Estimation using Feedforward Neural Networks with Lyapunov Stability Analysis. Defence Science Journal, 72 (5). pp. 655-664. ISSN 0011748X
Girija, G and Parameswaran, V and Raol, JR and Srinathkumar, S (1991) Estimation of lift and drag characteristics of an aircraft from flight data. Journal of Aeronautical Society of India, 43 (4). pp. 285-292.
Girija, G and Raol, JR (1993) Analysis of stabilised output error methods. Control Theory and Applications, IEE Proceedings, 143 (2). pp. 209-216. ISSN 1350-2379
Girija, G and Raol, JR (1996) Controller information based identification for unstable/augmented aircraft AIAA-96-0900. In: 34th Aerospace sciences meeting and exhibit, 15-18 Jan 1996, Reno, NV.
Girija, G and Raol, JR (1996) Estimation of aerodynamic parameters from dynamic maneuvers using estimation before modeling procedure. Jouranl of the Aeronautical Society of India, 48 (2). pp. 110-127. ISSN 0001-9267
Girija, G and Raol, JR (1992) PC Based Flight Path Reconstruction using UD Factorization Filtering Algorithm13; 13;. Technical Report. National Aerospace Laboratories, Bangalore, India.
Girija, G and Raol, JR (1993) PC-based flight path reconstruction using UD factorization filtering algorithm. Defence Science Journal, 43 (4). pp. 429-447.
Girija, G and Raol, JR and Appavu, Raj R and Kashyap, SK (2000) Tracking filter and multi-sensor data fusion. Sadhana, 25 (Part 2). pp. 159-167.
Gopal Ratnam, G and Raol, JR (1995) Estimation of parameters of unstable and augmented aircraft system using recursive mixed estimation technique. Journal of the Institution of Engineers (India): Aerospace Engineering Journal, 76. pp. 15-22.
Govindaraj, KS and Sridhar, JK and Madhuranath, Padma and Bhagawan, BS (1986) Six degree of freedom simulation software. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Goyal, Anup and Saraf, Amitabh and Pashilkar, AA and Patel, Ambalal V. (2011) Analysis of effect of wake vortices on air data sensors. In: Symposium on Applied Aerodynamics and Design of Aerospace Vehicle (SAROD 2011), November 16-18, 2011, Bangalore, India.
Hebbar, A and Pashilkar, AA (2016) Application of quantitative measures for analysing aircraft handling qualities. Defence Science Journal, 66 (1). pp. 3-10. ISSN 0011748X
Hebbar, PA and Pashilkar, AA and Biswas, P (2022) Using eye tracking system for aircraft design – a flight simulator study. Aviation, 26 (1). pp. 11-21. ISSN 16487788
Ismail, Shaik (2003) Large Transport Aircraft Handling Qualities. Project Report. National Aerospace Laboratories, Bangalore, India.
Ismail, Shaik and Chetty, Shyam (1991) Longitudinal equivalent system for augmented aircraft using modal decomposition/balanced reduction technique. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Ismail, Shaik and Pashilkar, AA and Ayyagari, Ramakalyan (2011) Adaptive control of micro air vehicles. In: Symposium on Applied Aerodynamics and Design of Aerospace Vehicle (SAROD 2011), November 16-18, 2011, Bangalore, India.
Ismail, Shaik and Pashilkar, AA and Ayyagari, Ramakalyan and Sundararajan, N (2013) Improved autolanding controller for aircraft encountering unknown actuator failures. In: IEEE Symposium Series on Computational Intelligence, 16 Apr 2013, Singapore.
Ismail, Shaik and Pashilkar, AA and Ayyagari, Ramakalyan (2015) Phase compensation and anti-windup design for neural-aided sliding mode fault-tolerant autoland controller. In: Cognitive Computing and Information Processing (CCIP), 2015 International Conference on, 3-4 March 2015, Noida, India.
Jain, S and Kamali, C and Goyal, Anup and Saraf, Amitabh (2022) A novel methodology to update table in air data system of a high performance fighter aircraft. Sadhana, 47 (39). pp. 1-17. ISSN 02562499
Jain, S and Kamali, C and Singh, GK (2019) Inertial Angle of Attack estimation for a small transport aircraft. In: 6th Indian Control Conference, ICC 2019, 18-20 December 2019, Hyderabad, India.
Jategaonkar, RV and Murthy, NN and Srinathkumar, S (1986) Aircraft parameter estimation, control and simulation (APECS) computers: An evaluation of quotations. Project Report. National Aerospace Laboratories, Bangalore.
Jategaonkar, RV and Plaetschke, E (1985) Maximum likelihood estimation of parameters in nonlinear flight mechanics systems. In: Conference on Identification and system parameter estimation 1985, 3-7 July 1985, United Kingdom.
Jatinder, Singh (1998) Parameter Estimation for Aircraft Flying in Turbulence. Technical Report. National Aerospace Laboratories, Bangalore, India.
Jayalakshmi, M and Patel, Vijay V and Singh, GK (2021) Relook at aileron to rudder interconnect. Defence Science Journal, 71 (2). pp. 153-161. ISSN 0011748X
Jebakumar, SK and Navendu, Kumar and Pashilkar, AA (2019) Flight Envelope Protection for a Fighter Aircraft. In: 2019 6th Indian Control Conference, ICC 2019, 18-20 December 2019, Hyderabad, India.
Jebakumar, SK and Pashilkar, A and Sundararajan, N (2022) A Novel Design Approach for Low-Speed Recovery of High-Performance Fighter Aircrafts. Defence Science Journal, 72 (4). pp. 505-515. ISSN 0011748X
Jigajinni, VS and Upendranath, V (2017) ANFIS-based fault diagnosis tool for a typical small aircraft fuel system. Advances in Intelligent Systems and Computing, 479. pp. 391-405. ISSN 21945357
Kamali, C and Bhogle, JR and Pashilkar, AA (1996) Implementation of real-time parameter estimation in LabVIEW and DSP. Journal of Aerospace Science and Technologies. pp. 353-397.
Kamali, C and Pashilkar, AA and Raol, JR (2007) Real time parameter estimation for reconfigurable control of unstable aircraft. Defence Science Journal. pp. 341-352.
Kamali, C and Jain, S and Saraf, Amitabh (2016) Novel method for static pressure calibration using Unscented Kalman Filter. IFAC-PapersOnLine, 49 (1). pp. 646-651. ISSN 24058963
Kamali, C and Ozger, E (2019) Limitations of Flight Path Reconstruction techniques. Sadhana - Academy Proceedings in Engineering Sciences, 44 (2). pp. 1-15. ISSN 02562499
Kannan, SM (1992) Evaluation of the dynamic stability characteristics of the NAL Light Transport Aircraft. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Kannan, SM (1999) A Study of the Dynamic Stability Characteristics of HANSA-3 Trainer Aircraft. Technical Report. National Aerospace Laboratories, Bangalore,India.
Kannan, SM and Rao, GNV (1987) The effect of periodic ballonet jet exhaust on the stability of a tethered aerostat AIAA-87-2504. In: AIAA 7th Lighter-than-Air technology conference.
Kannan, SM and Rao, GNV (1987) The effect of periodic ballonet jet exhaust on the stability of a tethered aerostat. In: 7th AIAA Lighter-Than Air Technology Conference, 17-19 Aug 1987, Monterey, United States.
Kashyap, SK and Girija, G (2009) EMRANN Controller for Aircraft Auto-Landing under Actuator Failure. In: UKIERI WORKSHOP NIT, 4-6 DECEMBER 2009, TIRCHY.
Kashyap, SK and Girija, G (2008) SENSOR FAULT TOLERANT CONTROL SYSTEM USING ONLINE MULTI-LAYER FEED-FORWARD NEURAL NETWORK. In: Tutorial cum Workshop on Robust Control of Smart Autonomous Unmanned Air Vehicles, 22-23 Aug 2008, IISc, Bangalore.
Kashyap, SK and Girija, G and Raol, JR (2006) Error model-converted measurement and error model-modified extended Kalman filters for target tracking. Defence Science Journal, 56 (5). pp. 679-692.
Kashyap, SK and Girija, G and Raol, JR (2004) Evaluation of Converted Measurement - and Modified13; Extended - Kalman Filters for Target Tracking. Project Report. National Aerospace Laboratories, Bangalore, India.
Kashyap, SK and Raol, JR (2006) Evaluation of derivative free Kalman filter and fusion in non-linear estimation. In: IEEE CCECE/CCGEI, May 2006, Ottawa.
Kashyap, SK and Raol, JR (2005) Performance evaluation of a fuzzy logic based Kalman filter for target tracking13;. In: 29th National Systems Conference (NSC 2005), 16-17 Dec 2005, IIT, Bombay.
Khadeeja Nusrath, TK and Basappa, Shri and Singh, Jatinder and Babu, GK (2017) In-Flight Center-of-Gravity Estimation Using Extended Kalman Filter. In: 2016 IEEE Annual India Conference, INDICON 2016, 16 - 18 December 2016, Bangalore, India.
Khadeeja Nusrath, TK and Singh, Jatinder (2020) Wind profile estimation during flight path reconstruction. Defence Science Journal, 70 (3). pp. 231-239. ISSN 0011748X
Khadeeja Nusrath, TK and lulu, V.P and Singh, J (2020) System identification of flybar-less rotorcraft UAV (2020) Aircraft Engineering and Aerospace Technology,. Aircraft Engineering and Aerospace Technology. ISSN 17488842
Khare, Alok and Madhuranath, Padma (1992) SOFT - Simulation of flight trajectories. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Khatri, AK (2011) Aircraft Turn Maneuver using Bifurcation Analysis and Nonlinear Dynamic Inversion Control Technique. In: NATIONAL CONFERENCE ON ADVANCED CONTROL IN ENGINEERING SYSTEMS , 21-23 September 2011, M.S.Ramaiah Institute of Technology, Bangalore.
Khatri, AK and Sinha, NK (2011) Aircraft Maneuver Design using Bifurcation Analysis and Nonlinear Control Techniques. In: 49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, 4-7 January, 2011, Orlando, Florida.
Khatri, AK and Kumar, Vineet (2016) Bifurcation analysis of a generic pusher type transport aircraft configuration in near-stall flight. In: 30th Congress of the International Council of the Aeronautical Sciences, ICAS 2016, 25-30 September 2016, Korea.
Kumar, Rajeev and Viswanath, PR (1997) The Influence of a Forward Splitter Plate on Base Pressure and Drag of Wedges. Technical Report. National Aerospace Laboratories, Bangalore, India.
Kumar, Shantha N and Jann, T (2002) Estimation of attitudes from a low cost miniaturized13; inertial platform using Kalman filter based sensor fusion algorithm. Technical Report. National Aerospace Laboratories, Bangalore, India.
Kumar, N and Deshpande, PJ and Dodamani, Ravi and Antony, R and Girish Prasad, M (2019) Interaction of two micro-propellers in coplanar and coaxial arrangement for UAV application. International Journal of Recent Technology and Engineering, 8 (2). pp. 5992-5995. ISSN 22773878
Kumar, Naresh and Nair, MT (2015) Suitability of density-corrected spalart-allmaras model for compression corner flows. Journal of Thermophysics and Heat Transfer, 29 (2). pp. 423-428. ISSN 08878722
Kumar, SS and Chotalia, RJ and Jana, S and Ganguli, Ranjan and Kandagal, SB (2019) Single stage axial compressor stability management with self-recirculating casing treatment. In: AIAA Scitech 2019 Forum, 7-11 January 2019, San Diego, California.
Lakshmi, P and Veena, S and Rahul, DK and Lokesha, H (2020) Speech interface for controlling micro air vehicle. Journal of Computational and Theoretical Nanoscience, 17 (1). pp. 488-491. ISSN 15461955
Lakshmikantha, Saraswathi and Murthy, NN and Adiga, BS (1986) Study of fixed point computations in implementing longitudinal axis flight controller. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Lathasree, P and Shaik , Ismil and Pashilkar, AA (2014) Design of Nonlinear Flight Controller for Fighter Aircraft. In: ACODS2014, 13 Mar 2014, IIT Kanpur.
Lathasree, P and Pashilkar, AA and Sundararajan, N (2019) Application of Generic Flight Controller Design Approach for A Delta Canard Fighter AircraftADMIRE. In: 6th Indian Control Conference, ICC 2019, 18-20 December 2019, Hyderabad, India.
Lokesha, H and Veena, S and Safiya, A and Ashwin Kumar, MP and Basavaraju, KS (2019) Evaluation of Delfino (TMS320F28379D) Processor for Helmet ANC Application. In: Global Conference for Advancement in Technology, GCAT 2019, 18-20 October 2019, Bengaluru, India.
Madhavan, Chinmayee and Dasannacharya, BS and Rajanna, D and Nagabhushana, S (1985) Aircraft weighing system. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Madhuranath, Padma and Niranjana, T (1987) Flight data analysis of the short period characteristics of pushpak aircraft. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Madhuranath, Padma and Sridhar, JK (1986) Simulation Study of Handling Characteristics of HS-748 with and Without Rotodome. Project Report. National Aerospace Laboratories, Bangalore.
Madhuranath, Padma and Sridhar, JK and Bhagavan, Satya B (1987) Simulation of a Light Aircraft. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Manoharan, LC and Muthuvel, S (1987) An intelligent fiberoptic data bus for fly-by-light applications. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Mathur, NB (1998) Correlation for the Estimation of Afterbody Drag with Hot Jet Exhaust. Journal of Aircraft, 35 (6). pp. 981-984.
Mathur, NB (1999) Estimation of afterbody drag with jet temperature effects for the afterbody-nozzle configuration of a combat aircraft. Journal of Aeronautical Society of India, 51 (3). pp. 181-185.
Mohamed, Majeed (2017) System identification of flexible aircraft in frequency domain. Aircraft Engineering and Aerospace Technology, 89 (6). pp. 826-834. ISSN 17488842
Mohamed, Majeed and Gopakumar, M (2021) Design of sliding mode flight control system for a flexible aircraft. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 236 (9). ISSN 09544100
Mohamed, Majeed and Joy, N (2021) Lateral directional aircraft aerodynamic parameter estimation using adaptive stochastic nonlinear filter. Aeronautical Journal, 125 (1294). 2217 -2228. ISSN 00019240
Mohamed, Majeed and Joy, N (2021) Nonlinear filter and neural modeling for calibration of aircraft airdata system. Journal of Aerospace Information Systems, 18 (12). pp. 949-963.
Mohamed, Majeed and Rong, S (2021) Neural Partial Differentiation-Based Estimation of Terminal Airspace Sector Capacity. SAE International Journal of Aerospace, 14 (2). p. 1. ISSN 19463855
Mohan Ram, VS and Raol, JR and Jagadeesh, M (1987) Flight Test Specification for Missile Parameter Identification. Project Report. National Aerospace Laboratories, Bangalore.
Mudkavi, Vidyadhar Y (2003) Powered Hang Gliding. Resonance, 8 (12). pp. 50-60.
Muralidhar, SJ and Balakrishna, S and Nagabhushana, S (1985) Evaluation of the acoustic modes of the 1100 CU.M. reverberation chamber. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Murthy, HS (1982) Subsonic and transonic roll damping measurements on Basic Finner (finned missile calibration model) AIAA-82-4042. Journal of Spacecraft and Rockets, 19. pp. 86-87. ISSN 0022-4650
Murthy, TVR and Seshadri, V (1994) Aid for mechanization of flight control systems on 13; micro-computers. Defence Science Journal, 44 (2). pp. 199-129. ISSN 0011-748X
Myala, J and Patel, Vijay V and Singh, GK (2019) Reliable Fault Identification for Aircraft Control Surface Damage. In: 6th Indian Control Conference, ICC 2019 - Proceedings, 18-20 December 2019, Hyderabad, India.
Myala, J and Patel, Vijay V and Singh, GK (2021) A non-iterative design for aileron to rudder interconnect gain. Aeronautical Journal, 125 (1286). pp. 763-774. ISSN 00019240
Naidu, VPS and Girija, G (2005) Acceleration and jerk models for tracking maneuvering targets. Technical Report. National Aerospace Laboratories, Bangalore, India.
Naidu, VPS and Girija, G and Raol, JR (2003) Determination of start and end points of a flight trajectory using UD filter and R-T-S smoother 13;. In: National Systems Conference - NSC, 17-19 Dec 2003, Kharagpur.
Naidu, VPS and Girija, G and Raol, JR (2003) Evaluation of Data Association and Fusion13; Algorithms for Tracking in the Presence of13; Measurement Loss. Project Report. National Aerospace Laboratories, Bangalore, NAL.
Naidu, VPS and Raol, JR (2007) Target tracking with multi acoustic array sensors data. Defence Science Journal, 57 (3). pp. 289-303.
Onkar, AK (2021) A successive robust flutter prediction technique for aeroelastic systems using µ method. Meccanica, 56 (10). pp. 2613-2629. ISSN 00256455
Padma, A and Rao, RMVGK and Subramaniam, C and Nagendrappa, G (1995) Cure characterization of triglycidyl epoxy/aromatic amine systems. Journal of Applied Polymer Science, 57 (4). pp. 401-411.
Padma, Madhuranath and Sridhar, JK and Satyabhagavan, B and Krishnamurthy, KK (1987) Basic Data required for the Lockheed Real Time Simulation of HS - 748 Aircraft. Project Report. National Aerospace Laboratories, Bangalore.
Parameswaran, V and Girija, G and Raol, JR (2003) Estimation of parameters from large amplitude maneuvers13; with partitioned data for aircraft. Project Report. National Aerospace Laboratories, Bangalore, India.
Parameswaran, V and Jategaonkar, RV and Press, M (2005) Five-Hole Flow Angle Probe Calibration from Dynamic and Tower Flyby Maneuvers. Journal of Aircraft, 42 (1). pp. 80-86. ISSN 0021-8669
Parameswaran, V and Raol, JR and Ismail, Shaik (1991) Parameter estimation via nonlinear differential correction least square method. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Pashilkar, AA (2007) Development of Saras Autopilot. In: Symposium on Aircraft Design, 14th June 2007, Bangalore, India.
Pashilkar, AA (2005) Enhanced Fault-Tolerant Neural Controller for Aircraft Auto-Landing. Technical Report. National Aerospace Laboratories, Bangalore, India.
Pashilkar, AA and Haijun, Rong and Sundararajan, N and Saratchandran, P (2011) Fault toleranat neuro/neuro-fuzzy controllers for aircraft auto landing with actuator failures and severe winds. In: Symposium on Applied Aerodynamics and Design of Aerospace Vehicle (SAROD 2011), November 16-18, 2011, Bangalore, India.
Pashilkar, AA and Ismail, Shaik and Ayyagari, Ramakalyan and Sundararajan, N (2013) Design of a nonlinear dynamic inversion controller for trajectory following and maneuvering for fixed wing aircraft. In: IEEE Symposium Series on Computational Intelligence, 16 Apr 2013, Singapore.
Pashilkar, AA and Sundararajan, N and Saratchandran, P (2005) Adaptive backstepping neural controller for aircraft autolanding. Technical Report. National Aerospace Laboratories, Bangalore, India.
Pashilkar, AA and Sundararajan, N and Saratchandran, P (2007) Adaptive nonlinear neural controller for aircraft under actuator failures. Journal of Guidance, Control and Dynamics, 30 (3). pp. 835-847. ISSN 1533-3884
Pedar, A and Santharam, A and Nagaraja, G (1992) quot;Application of Al in Reconfigurable Flight Control Systemsquot;. Technical Report. National Aerospace Laboratories, Bangalore, India.
Prakash, Shashikala and Renjith kumar, TG and Raja, S and Dwarakanathan, D and Subramani, H and Karthikeyan, C (2016) Active vibration control of a full scale aircraft wing using a reconfigurable controller. Journal of Sound and Vibration, 361. pp. 32-49. ISSN 0022460X
Prasad, S Ganesh and Premalatha, and Ramamoorthy, P (1991) Small Aircraft Stability and Response Analysis (SASTRA). Technical Report. National Aerospace Laboratories, Bangalore, India.
Raghavendra, K and Madan, M and Venkatesh, V and Sujata, M and Bhaumik, S K (2022) Failure Analysis of a Welded AISI321 Steel Bleed Air Connector of an Aircraft Engine. Journal of Failure Analysis and Prevention, 22 (4). pp. 1776-1786. ISSN 15477029
Raghavendra Rao, S and Ravishankar, S (2015) Optimization of Actuating Mechanisms of Flight Control Surfaces through Computer Aided Kinematics. In: ARMS-2015, 30th - 31st January 2015, ISRO, Bangalore.
Rajamurthy, MS (2002) Modelling of the nonlinear lift and pitching moment characteristics of 60-degree delta wing and wing-bodies. In: AIAA Atmospheric Flight Mechanics Conference and Exhibit, 5-8 Aug 2002, Monterey, California, United States.
Rajamurthy, MS (1988) Stability and control derivatives of Light Canard Research Aircraft (LCRA). Technical Report. National Aeronautical Laboratory, Bangalore, India.
Rajamurthy, MS and Basappa, - (1991) NALLA 1 Longitudinal stick-free stability. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Raju, J and Duragkar, MS and Jagannathan, N and Manjunatha, CM (2014) Prediction of Onset of Mode I Delamination Growth Under a Tensile Spectrum Load. Journal of Materials Science Research, 3 (2). pp. 44-51. ISSN 1927-0593
Raju, RG and Kashyap, SK (2020) 3D Localisation of Target using Elevation Angle Algorithm with the use of Ground Radars. Defence Science Journal, 70 (3). pp. 260-271. ISSN 0011748X
Ramabhadran, S and Sridharan, R (1982) Computation of the aerodynamic characteristics of wings in linearised supersonic flow. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Ramamoorthy, P (1989) Extended Kalman Filter Algorithm (EKF). Technical Report. National Aerospace Laboratories, Bangalore, India.
Ramamoorthy, P and Sinha, AK and Narayana, CL and Dutta, Vimala and Dwarakanath, GS and Sheela, BV (1976) Optimization of a passenger aircraft for minimum direct operating cost - A preliminary study. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Ramamurthi, G and Bandyopadhyay, B and Arya, H and Singh, GK (2016) Tracking control for nonminimum phase MIMO micro aerial vehicle - A dynamic sliding manifold approach. Proceedings of the Institution of Mechanical Engineers. Part I: Journal of Systems and Control Engineering, 230 (9). pp. 1001-1029. ISSN 09596518
Ramamurthy, TV (1988) An automated aid for microcomputer implementation of flight control systems. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Rao, RMVGK (1991) Composite materials indigenisation for FRP - Air crafts. Technical Report. National Aerospace Laboratories, Bangalore, India.
Rao, Raghavendra S and Ravishankar, S (2010) Kinematic Analysis of a Track Link Mechanism For Trailing Edge Flaps of Aircraft. In: 7th National Seminar & Exhibition on Aerospace And Related MEchanisms ARMS-2010, 17th & 18th September 2010, Thiruvananthapuram, Kerala, India..
Rao, ANV and Satish, TN and Naidu, VPS and Jana, S (2022) Machine learning augmented multi-sensor data fusion to detect aero engine fan rotor blade flutter. International Journal of Turbo and Jet Engines. ISSN 03340082
Raol, JR (2004) Multi-source multi-sensor information fusion. Sadhana - Academy Proceedings in Engineering Sciences, 29 (2). pp. 143-144.
Raol, JR and Desai, RC (1976) State estimation for discrete system with time delay using invariant embedding - Part II. Institution of Engineers (India) Journal, 56. pp. 70-72.
Raol, JR and Girija, G (2001) Evaluation of adaptive Kalman filtering methods for target tracking applications. In: AIAA Guidance, Navigation, and Control Conference and Exhibit, 6-9 Aug 2001, Montreal, United States.
Raol, JR and Girija, G (1999) Modelling and parameter estimation for fly-by-wire aircraft/control systems. Sadhana, 24 (part 1). pp. 97-119.
Raol, JR and Gopalratnam, G (1996) Analysis of stabilised output error methods. IEE Proceedings: Control Theory and Applications, 143 (2). pp. 209-216.
Raol, JR and Gopalratnam, G (1996) Approach to parameter estimation of unstable systems. Institution of Engineers (India) Journal-EL, 77. pp. 207-211.
Raol, JR and Jategaonkar, RV (1995) Aircraft parameter estimation using recurrent neural networks - A critical appraisal. In: AIAA Atmospheric Flight Mechanics Conference, 7-9 Aug 1995, Maryland, United States.
Sahoo, PK and Dattaguru, B and Manjunatha, CM (2017) Strength Prediction of Adhesively Bonded Joints using Plastic Zone Size Criterion. In: Procedia Engineering.
Santharam, A (1988) Model Following control for a Light Combat Aircraft. Project Report. NAL, Bangalore.
Santharam, A (1991) Reconfigurable control law. Project Report. National Aerospace Laboratories, Bangalore.
Saraswathi, L and Chetty, Shyam (1990) Longitudinal equivalent system for augmented aircraft using least square curve fitting technique. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Sarma, GR (1983) Nonlinear filter for pilot's remnant attenuation. Journal of Guidance, Control and Dynamics, 6 (2). pp. 123-124. ISSN 0731-5090
Sarma, GR and Bapat, YN (1976) Analysis of visual threshold effect on manual aircraft control. Journal of Aircraft, 13 (4). pp. 225-226. ISSN 0021-8669
Savanur, Shobha R. and Kashyap, SK and Raol, JR (2008) Adaptive Neuro-Fuzzy Based Sensor Fault Detection, Isolation and Reconfiguration. Journal of Systems Science and Engineering, System Society of India, 17 (1). ISSN 0972-5032
Shankar, Vijayalaxmi and Pedar, A (1990) FLEXIBUS - Multinode Flexible Cable Bus Specifications - Version 1. Project Report. National Aerospace Laboratories, Bangalore.
Shankar, Vijayalaxmi and Pedar, A and Nadagowda, RV and Jayasree, BS (1990) Performance Evaluation of FLEXIBUS through modelling & Simulation. Project Report. National Aerospace Laboratories, Bangalore.
Shantha Kumar, N (1990) Aerodynamic Parameter Estimation for Prithvi from first Flight Test Data:Preliminary Result 2. Technical Report. NAL.
Shantha Kumar, N (2002) Estimation of Attitudes from a Low Cost Miniaturized Inertial Platform using Kalman Filter based Sensor Fusion Algorithm. Technical Report. NAL.
Shantha Kumar, N (1999) Input Excitation Techniques for Aerodynamics Derivatives Estimation of Highly Augmented Fighter Aircraft. Defence Science journal. pp. 187-196. ISSN 0011-748X
Shantha Kumar, N (1996) A Software Tool for Parameter Estimation from Flight Test Data. In: MATLAB Users Conference 1996, Bangalore.
Shantha Kumar, N (2001) Stability and control derivatives of LCRA from flight data. Technical Report. NAL.
Shantha Kumar, N and Jann, T (2004) Estimation of attitudes from a low-cost miniaturized inertial platform using Kalman Filter-based sensor fusion algorithm. Sadhana - Academy Proceedings in Engineering Sciences, 29 (2). pp. 217-235.
Shantha Kumar, N and Kashyap, SK (2006) Target Tracking in Non-Gaussian Environment. In: National Conference on Range Technology.
Shantha Kumar, N and Raol, JR (1998) Lateral Directional Parameter Estimation of Fly-by-wire Aircraft and Validation using simulation data. Technical Report. NAL, Bangalore.
Shantha Kumar, N and Raol, JR and Balakrishna, S (1989) Aerodynamic Parameter Estimation for Prithvi from first Flight Test Data:Preliminary Result. Technical Report. NAL.
Shantha Kumar, N and Raol, JR and Balakrishna, S (1991) Feasibility study of Analysing ASLVD2 flight data estimation of Aerodynamic Derivatives. Technical Report. NAL.
Shantha Kumar, N and Raol, JR and Balakrishna, S and Girija, G (1990) Estimation of aerodynamic derivatives from free flight trajectory of aeroballistic range using maximum likelihood method. Technical Report. NAL.
Shantha kumar, N and Girija, G and Raol, JR (2004) Seeker Filter and Fusion for Maneuvering Target using IMM. Project Report. National Aerospace Laboratories, Bangalore.
Shariff, Hina and Lathasree, P (2005) Nonlinear Modeling of Wind Tunnel Database for a Fighter Aircraft. Technical Report. National Aerospace Laboratories, Bangalore, India.
Shibu, PS and Sandeep, - and Choudhury, Balamati and Nair, RU (2021) Multi-objective Optimization Approach for Low RCS Aerodynamic Design of Aerospace Structures. In: Design and Development of Aerospace Vehicles and Propulsion Systems, Singapore.
Shyam, Chetty (2004) Design and Development of Flight Control Laws for LCA Airforce Variants - FSED Phase II, Part 2. Project Report. National Aerospace Laboratories, Bangalore.
Shyam, Chetty and Raol, JR (1992) Computer aided evaluation aircraft handling qualities and flight control system robustness. In: AIAA atmospheric flight mechanics conference.
Singh, AK and Jayaraman, A and Chatterjee, A (1971) Pressure induced electronic and NaCl to CsCl type transitions in some rare earth monotellurides. Solid State Communications, 9 (1). pp. 1459-1462.
Singh, Jatinder and Girija, G (1998) Identification of helicopter rigid body dynamics from flight data. Defence Science journal, 48 (1). pp. 69-86. ISSN 0011-748X
Singh, Jatinder and Kashyap, SK (2002) Interacting Multiple Model Approach for Tracking13; Maneuvering Targets. Project Report. National Aerospace Laboratories, Bangalore, India.
Singh, Jatinder and Kashyap, SK and Girija, G and Raol, JR (2002) Interacting multiple model approach for target tracking and trajectory estimation. In: National Conference on Sensor Technology, 26-27 Sep 2002, Delhi, India.
Srinatha Sastry, CV and Sathyabhagavan, B and Raol, JR and Sinha, NK (1990) A scheme for sensor failure management using observers and knowledge based approach. Technical Report. National Aerospace Laboratories, Bangalore, India.
Srinatha Sastry, CV and Satyabhagavan, B and Raol, JR and Sinha, NK (1992) Knowledge based sensor failure management using observers. In: Fifteenth National Systems Conference, 13-15 Mar 1992, Roorkee, India.
Srinathkumar, S and Parameswaran, V and Girija, G (1986) Estimation of teh longitudinal stability characteristics of MiG-21BIS aircraft from flight data. Project Report. National Aerospace Laboratories, Bangalore.
Srinathkumar, S and Parameswaran, V and Girija, G (1986) Estimation of the longitudinal stability characterisiticvs of MIG 21BIS Aircraft from Flight DATA. Project Report. National Aerospace Laboratories, Bangalore.
Srinathkumar, S and Parameswaran, V and Raol, JR (1995) Flight test determination of neutral and maneuver points of aircraft. In: AIAA Atmospheric Flight Mechanics Conference, 3, Baltimore, United States.
Srinathkumar, S and Srinatha Sastry, CV (1982) On the use of modal sensitivity measures in flight control applications. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Srinathkumar, S and Waszak, Martin R (1992) Active flutter suppression using dipole filters. Technical Report. National Aeronautical Laboratories, Bangalore, India.
Srinathkumar, S (2019) Rotorcraft precision hover control in atmospheric turbulence via eigenstructure assignment. Journal of the American Helicopter Society, 64 (1). pp. 1-12. ISSN 00028711
Srinivas, K (1980) Computation of steady supersonic flows - two dimentional and axisymmetric13;. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Subaschandar, N and Prabhu, A (1998) Analysis of turbulent near-wake development behind an infinitely yawed flat plate. International Journal for Non-Linear Mechanics, 33 (6). pp. 1089-1109.
Subramanian, NR and Ramakrishnan, SV (1977) Dynamic stability derivatives of missile configurations (Theoretical evaluation). Technical Report. National Aeronautical Laboratory, Bangalore, India.
Sudeesh , PD and Kashyap, SK and Kayalvizhi, R (2008) A SCHEME OF SFDIA USING MULTILAYER PERCEPTRON AND EBP FOR UNMANNED AERIAL VEHICLE. In: International Conference on Aerospace Science and Technology (INCAST 2008-094), 26-28 Jun 2008, Bangalore, India.
Sudesh, K Kashyap and Girija, G Fuzzy Controller for Aircraft Auto-Landing. In: Robust Control of Smart Autonomous Unmanned Air Vehicle under United Kingdom India Education and Research Initiative (UKIERI) program, December 2010, IIT, Bombay, Mumbai.
Sudhakar, S and Karthikeyan, N (2021) Flow Separation Control on a NACA-4415 Airfoil at Low Reynolds Number. In: Proceedings of 16th Asian Congress of Fluid Mechanics, Singapore.
Sudheera, - and Rammohan, Y.S. and Pradeep, M.S. (2018) Split Hopkinson Pressure Bar Apparatus for Compression Testing: A Review. In: Materials Today: Proceedings.
Sujata, M and Madan, M and Raghavendra, K and Jagannathan, N and Bhaumik, SK Unraveling the cause of an aircraft accident. Engineering Failure Analysis, 97. pp. 740-758. ISSN 13506307
Sundaram, P and Sengupta, S and Suman, V K and Sengupta, T K and Bhumkar, Y G and Mathpal, R K (2022) Flow control using single dielectric barrier discharge plasma actuator for flow over airfoil. Physics of Fluids, 34 (9). pp. 1-22. ISSN 10706631
Sunder, R and Prakash, Raghu V (1994) A Study of Fatigue Crack Growth in Lugs Under Spectrum Loading. Technical Report. National Aerospace Laboratories, Bangalore, India.
Suresh, S and Naidu, VPS (2021) Mahalanobis-ANOVA criterion for optimum feature subset selection in multi-class planetary gear fault diagnosis. Journal of Vibration and Control, 28 (21-22). pp. 3257-3268. ISSN 10775463
Suryanarayana, BG (1974) Design of a sidewall-mounted model incidence system for the N.A.L. l' X l' Trisonic Wind Tunnel. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Thomas, Moncy T and Nagaraj, S (1994) Data Acquisition and Inter Process Communication13; for Engineer-in-the-Loop Simulator (ELS). Technical Report. National Aerospace Laboratories, Bangalore, India.
Vaitheeswaran, SM and Mekala, R (2015) Non-linear attitude control methods for quadrotor MAVs-A study. In: Cognitive Computing and Information Processing (CCIP), 2015 International Conference on, 3-4 March 2015, Noida, India.
Varughese, Byji and Dayananda, GN and Subba Rao, M (2008) Modeling the behaviour of an advanced material based smart landing gear system for aerospace vehicles. In: International Workshop on quot;Smart deeling of Material Systems (SDMoMS'08), Jan 2008, Chennai, India.
Varute, PT (1986) Estimates of longitudinal and lateral stability and control characteristics of Pushpak Aircraft. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Varute, PT (1990) Precision mechanics of actuators in aircraft and rockets. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Varute, PT and Gnanesh, N (1991) NALLA prototype flight envelope. Technical Report. National Aerospace Laboratories, Bangalore, India.
Vepa, Ranjan (1979) Comment on 'active flutter control using generalized unsteady13; aerodynamic theory'. Journal of Guidance and Control, 2. pp. 446-447.
Verma, SB and Manisankar, C (2012) Shockwave/boundary-layer interaction control on a compression ramp using steady microjet. AIAA Journal, 50 (12). pp. 2753-2764. ISSN 0001-1452
Vinay, CA and Chakravarthy, B (2017) Aerothermal analysis of insulation to protect exhaust ducts of a pusher turbo prop engine aircraft. Lecture Notes in Mechanical Engineering, PartF8. pp. 843-851. ISSN 21954356
Viswanath, PR and Mukund, R (1995) Turbulent drag reduction using riblets on a supercritical airfoil at transonic speeds. AIAA Journal, 33 (5). pp. 945-947.
Vyas, JJ and Balamurugan, G and Rakesh, M (2016) Simulation of typical civil aircraft fuel transfer process. In: NUiCONE 2015 - 5th Nirma University International Conference on Engineering, 26-28 Novermber 2016, Ahmedabad, India.
Waszak, Martin R and Srinathkumar, S (1992) Design and experimental validation of a flutter suppression controller for the active flexible wing. Technical Report. National Aeronautics and Space Administration, USA.
Waszak, Martin R and Srinathkumar, S (1992) Flutter suppression for the active flexible wing: Control system design and experimental validation AIAA-92-2097. In: Dynamics specialists conference.
