Items where Subject is "AERONAUTICS > Aircraft Stability and Control"

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Number of items at this level: 139.

Conference or Workshop Item

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.

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.

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.

Goyal, Anup and Saraf, Amitabh and Pashilkar, A 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.

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.

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.

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 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.

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.

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.

Pashilkar, A. A 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, Abhay (2007) Development of Saras Autopilot. In: Symposium on Aircraft Design, 14th June 2007, Bangalore, India.

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.

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..

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 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.

Shantha Kumar, N (1996) A Software Tool for Parameter Estimation from Flight Test Data. In: MATLAB Users Conference 1996, Bangalore.

Shantha Kumar, N and Kashyap, SK (2006) Target Tracking in Non-Gaussian Environment. In: National Conference on Range Technology.

Shyam, Chetty and Raol, JR (1992) Computer aided evaluation aircraft handling qualities and flight control system robustness. In: AIAA atmospheric flight mechanics conference.

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 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 Parameshwaran, 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.

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.

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.

Waszak, MR and Srinathkumar, S (1992) Flutter suppression for the active flexible wing: Control system design and experimental validation AIAA-92-2097. In: Dynamics specialists conference.

Journal Article

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) 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 (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, Sudesh (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.

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.

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.

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.

Mudkavi, Vidyadhar Y (2003) Powered Hang Gliding. Resonance, 8 (12). pp. 50-60.

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

Naidu, VPS and Raol, JR (2007) Target tracking with multi acoustic array sensors data. Defence Science Journal, 57 (3). pp. 289-303.

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.

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

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

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 (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.

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

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 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.

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

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.

Vepa, R (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

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.

Proj.Doc/Technical Report

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.

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.

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.

Chetty, Shyam (1988) Design of robust flight control systems. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Dhanalakshmi, K and Mathur, JS and Chakrabartty, SK (2003) Radomes for JAGUAR aircraft: Closure Report. Technical Report. National Aerospace Laboratories, Bangalore.

Girija, G and Raol, JR (1992) PC Based Flight Path Reconstruction using UD Factorization Filtering Algorithm13; 13;. Technical Report. National Aerospace Laboratories, Bangalore, India.

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.

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.

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.

Jatinder, Singh (1998) Parameter Estimation for Aircraft Flying in Turbulence. Technical Report. National Aerospace Laboratories, Bangalore, India.

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.

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.

Khare, Alok and Madhuranath, Padma (1992) SOFT - Simulation of flight trajectories. Technical Report. National Aeronautical Laboratory, Bangalore, India.

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.

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.

Madhavan, Chinmayee and Dasannacharya, BS and Rajanna, D and Nagabhushana, S (1985) Aircraft weighing system. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Madhuranath, P 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.

Mohan Ram, VS and Raol, JR and Jagadeesh, M (1987) Flight Test Specification for Missile Parameter Identification. Project Report. National Aerospace Laboratories, Bangalore.

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.

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) Evaluation of Data Association and Fusion13; Algorithms for Tracking in the Presence of13; Measurement Loss. Project Report. National Aerospace Laboratories, Bangalore, NAL.

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 Raol, JR and Ismail, Shaik (1991) Parameter estimation via nonlinear differential correction least square method. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Pashilkar, AA (2005) Enhanced Fault-Tolerant Neural Controller for Aircraft Auto-Landing. Technical Report. National Aerospace Laboratories, Bangalore, India.

Pashilkar, AA and Sundararajan, N and Saratchandran, P (2005) Adaptive backstepping neural controller for aircraft autolanding. Technical Report. National Aerospace Laboratories, Bangalore, India.

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.

Prasad, S Ganesh and Premalatha, and Ramamoorthy, P (1991) Small Aircraft Stability and Response Analysis (SASTRA). Technical Report. National Aerospace Laboratories, Bangalore, India.

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.

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.

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.

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.

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 (2001) Stability and control derivatives of LCRA from flight data. Technical Report. NAL.

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.

Shanthakumar, 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.

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.

Singh, Jatinder and Kashyap, Sudesh (2002) Interacting Multiple Model Approach for Tracking13; Maneuvering Targets. Project Report. National Aerospace Laboratories, Bangalore, 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.

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 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.

Srinivas, K (1980) Computation of steady supersonic flows - two dimentional and axisymmetric13;. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Subramanian, NR and Ramakrishnan, SV (1977) Dynamic stability derivatives of missile configurations (Theoretical evaluation). Technical Report. National Aeronautical Laboratory, Bangalore, India.

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.

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.

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.

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.

This list was generated on Wed Jul 23 01:04:01 2014 IST.