Subject: Aircraft Stability and Control

• NASA Aerospace Subject Categories (3081)
  • AERONAUTICS (1325)
    • Aircraft Stability and Control (101)

Number of records: 101.

[] 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 "Smart deeling of Material Systems (SDMoMS'08), Jan 2008, Chennai, India.
[Department(s): Advanced Composites Division, Advanced Composites Division, Advanced Composites Division] ["page:no_fulltext_short" not defined]

[] Naidu, VPS and Raol, JR (2007) Target tracking with multi acoustic array sensors data. Defence Science Journal, 57 (3). pp. 289-303.
[Department(s): Flight Mechanics and Control Division, Flight Mechanics and Control Division]

[] 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
[Department(s): Flight Mechanics and Control Division, Flight Mechanics and Control Division, Flight Mechanics and Control Division] ["page:no_fulltext_short" not defined]

[] Ananda, CM (2007) Civil Aircraft Advanced Avionics Architecutres - An Insight Into Saras Avionics, Present and Future Perspective. In: Symposium on Aircraft Design, 14th June 2007, Bangalore, India.
[Department(s): Aerospace Electronics and Controls Division]

[] Pashilkar, Abhay (2007) Development of Saras Autopilot. In: Symposium on Aircraft Design, 14th June 2007, Bangalore, India.
[Department(s): Flight Mechanics and Control Division]

[] 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.
[Department(s): Flight Mechanics and Control Division, Other, Flight Mechanics and Control Division] ["page:no_fulltext_short" not defined]

[] 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.
[Department(s): Flight Mechanics and Control Division, Flight Mechanics and Control Division, Flight Mechanics and Control Division]

[] 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.
[Department(s): Flight Mechanics and Control Division, Flight Mechanics and Control Division]

[] Pashilkar, AA and Sundararajan, N and Saratchandran, P (2005) Adaptive backstepping neural controller for aircraft autolanding. Technical Report. National Aerospace Laboratories, Bangalore, India.
[Department(s): Flight Mechanics and Control Division, Flight Mechanics and Control Division, Flight Mechanics and Control Division]

[] Shariff, Hina and Lathasree, P (2005) Nonlinear Modeling of Wind Tunnel Database for a Fighter Aircraft. Technical Report. National Aerospace Laboratories, Bangalore, India.
[Department(s): Flight Mechanics and Control Division, Flight Mechanics and Control Division]

[] Pashilkar, AA (2005) Enhanced Fault-Tolerant Neural Controller for Aircraft Auto-Landing. Technical Report. National Aerospace Laboratories, Bangalore, India.
[Department(s): Flight Mechanics and Control Division]

[] Naidu, VPS and Girija, G (2005) Acceleration and jerk models for tracking maneuvering targets. Technical Report. National Aerospace Laboratories, Bangalore, India.
[Department(s): Flight Mechanics and Control Division, Flight Mechanics and Control Division]

[] 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
[Department(s): Flight Mechanics and Control Division, Other, Other] ["page:no_fulltext_short" not defined]

[] Kashyap, SK and Raol, JR (2005) Performance evaluation of a fuzzy logic based Kalman filter for target tracking. In: 29th National Systems Conference (NSC 2005), 16-17 Dec 2005, IIT, Bombay.
[Department(s): Flight Mechanics and Control Division, Flight Mechanics and Control Division]

[] 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.
[Department(s): Flight Mechanics and Control Division]

[] Kashyap, SK and Girija, G and Raol, JR (2004) Evaluation of Converted Measurement - and Modified Extended - Kalman Filters for Target Tracking. Project Report. National Aerospace Laboratories, Bangalore, India.
[Department(s): Flight Mechanics and Control Division, Flight Mechanics and Control Division, Flight Mechanics and Control Division]

[] 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.
[Department(s): Flight Mechanics and Control Division, Other] ["page:no_fulltext_short" not defined]

[] Raol, JR (2004) Multi-source multi-sensor information fusion. Sadhana - Academy Proceedings in Engineering Sciences, 29 (2). pp. 143-144.
[Department(s): Flight Mechanics and Control Division] ["page:no_fulltext_short" not defined]

[] 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. In: National Systems Conference - NSC, 17-19 Dec 2003, Kharagpur.
[Department(s): Flight Mechanics and Control Division, Flight Mechanics and Control Division, Flight Mechanics and Control Division]

[] Mudkavi, Vidyadhar Y (2003) Powered Hang Gliding. Resonance, 8 (12). pp. 50-60.
[Department(s): Computational and Theoretical Fluid Dynamics Division]

[] Parameswaran, V and Girija, G and Raol, JR (2003) Estimation of parameters from large amplitude maneuvers with partitioned data for aircraft. Project Report. National Aerospace Laboratories, Bangalore, India.
[Department(s): Flight Mechanics and Control Division, Flight Mechanics and Control Division, Flight Mechanics and Control Division]

[] Naidu, VPS and Girija, G and Raol, JR (2003) Evaluation of Data Association and Fusion Algorithms for Tracking in the Presence of Measurement Loss. Project Report. National Aerospace Laboratories, Bangalore, NAL.
[Department(s): Flight Mechanics and Control Division, Flight Mechanics and Control Division, Flight Mechanics and Control Division]

[] Ismail, Shaik (2003) Large Transport Aircraft Handling Qualities. Project Report. National Aerospace Laboratories, Bangalore, India.
[Department(s): Flight Mechanics and Control Division]

[] Kumar, Shantha N and Jann, T (2002) Estimation of attitudes from a low cost miniaturized inertial platform using Kalman filter based sensor fusion algorithm. Technical Report. National Aerospace Laboratories, Bangalore, India.
[Department(s): Flight Mechanics and Control Division, Flight Mechanics and Control Division]

[] 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.
[Department(s): Flight Mechanics and Control Division, Flight Mechanics and Control Division, Flight Mechanics and Control Division, Flight Mechanics and Control Division]

[] 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.
[Department(s): Flight Mechanics and Control Division] ["page:no_fulltext_short" not defined]

[] Singh, Jatinder and Kashyap, Sudesh (2002) Interacting Multiple Model Approach for Tracking Maneuvering Targets. Project Report. National Aerospace Laboratories, Bangalore, India.
[Department(s): Flight Mechanics and Control Division, Flight Mechanics and Control Division]

[] 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.
[Department(s): Flight Mechanics and Control Division, Flight Mechanics and Control Division] ["page:no_fulltext_short" not defined]

[] 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.
[Department(s): Flight Mechanics and Control Division, Flight Mechanics and Control Division, Other, Flight Mechanics and Control Division]

[] Kannan, SM (1999) A Study of the Dynamic Stability Characteristics of HANSA-3 Trainer Aircraft. Technical Report. National Aerospace Laboratories, Bangalore,India.
[Department(s): Experimental Aerodynamics Division]

[] 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.
[Department(s): Experimental Aerodynamics Division]

[] Raol, JR and Girija, G (1999) Modelling and parameter estimation for fly-by-wire aircraft/control systems. Sadhana, 24 (part 1 & 2). pp. 97-119.
[Department(s): Flight Mechanics and Control Division, Flight Mechanics and Control Division]

[] Jatinder, Singh (1998) Parameter Estimation for Aircraft Flying in Turbulence. Technical Report. National Aerospace Laboratories, Bangalore, India.
[Department(s): Flight Mechanics and Control Division]

[] Mathur, NB (1998) Correlation for the Estimation of Afterbody Drag with Hot Jet Exhaust. Journal of Aircraft, 35 (6). pp. 981-984.
[Department(s): Experimental Aerodynamics Division]

[] 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
[Department(s): Flight Mechanics and Control Division, Flight Mechanics and Control Division] ["page:no_fulltext_short" not defined]

[] 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.
[Department(s): Experimental Aerodynamics Division, Other]

[] 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.
[Department(s): Experimental Aerodynamics Division, Experimental Aerodynamics Division]

[] 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
[Department(s): Flight Mechanics and Control Division, Flight Mechanics and Control Division] ["page:no_fulltext_short" not defined]

[] Raol, JR and Gopalratnam, G (1996) Analysis of stabilised output error methods. IEE Proceedings: Control Theory and Applications, 143 (2). pp. 209-216.
[Department(s): Flight Mechanics and Control Division, Flight Mechanics and Control Division]

[] Raol, JR and Gopalratnam, G (1996) Approach to parameter estimation of unstable systems. Institution of Engineers (India) Journal-EL, 77. pp. 207-211.
[Department(s): Flight Mechanics and Control Division, Flight Mechanics and Control Division] ["page:no_fulltext_short" not defined]

[] 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.
[Department(s): Flight Mechanics and Control Division, Flight Mechanics and Control Division]

[] 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.
[Department(s): Flight Mechanics and Control Division, Other, Flight Mechanics and Control Division] ["page:no_fulltext_short" not defined]

[] 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.
[Department(s): Flight Mechanics and Control Division, Other]

[] 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.
[Department(s): Flight Mechanics and Control Division, Flight Mechanics and Control Division, Flight Mechanics and Control Division] ["page:no_fulltext_short" not defined]

[] 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.
[Department(s): Other, Flight Mechanics and Control Division, Other, Other] ["page:no_fulltext_short" not defined]

[] 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.
[Department(s): Experimental Aerodynamics Division, Experimental Aerodynamics Division] ["page:no_fulltext_short" not defined]

[] 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.
[Department(s): Flight Mechanics and Control Division, Flight Mechanics and Control Division] ["page:no_fulltext_short" not defined]

[] Thomas, Moncy T and Nagaraj, S (1994) Data Acquisition and Inter Process Communication for Engineer-in-the-Loop Simulator (ELS). Technical Report. National Aerospace Laboratories, Bangalore, India.
[Department(s): Flight Mechanics and Control Division, Flight Mechanics and Control Division]

[] 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.
[Department(s): Structural Integrity Division, Structural Integrity Division]

[] Murthy, TVR and Seshadri, V (1994) Aid for mechanization of flight control systems on micro-computers. Defence Science Journal, 44 (2). pp. 199-129. ISSN 0011-748X
[Department(s): Other, Experimental Aerodynamics Division] ["page:no_fulltext_short" not defined]

[] Girija, G and Raol, JR (1993) PC-based flight path reconstruction using UD factorization filtering algorithm. Defence Science Journal, 43 (4). pp. 429-447.
[Department(s): Flight Mechanics and Control Division, Flight Mechanics and Control Division]

[] 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
[Department(s): Flight Mechanics and Control Division, Flight Mechanics and Control Division]

[] Kannan, SM (1992) Evaluation of the dynamic stability characteristics of the NAL Light Transport Aircraft. Technical Report. National Aeronautical Laboratory, Bangalore, India.
[Department(s): Experimental Aerodynamics Division]

[] Khare, Alok and Madhuranath, Padma (1992) SOFT - Simulation of flight trajectories. Technical Report. National Aeronautical Laboratory, Bangalore, India.
[Department(s): Flight Mechanics and Control Division, Flight Mechanics and Control Division]

[] 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.
[Department(s): Flight Mechanics and Control Division, Flight Mechanics and Control Division, Flight Mechanics and Control Division]

[] 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.
[Department(s): Other, Flight Mechanics and Control Division]

[] Pedar, A and Santharam, A and Nagaraja, G (1992) "Application of Al in Reconfigurable Flight Control Systems". Technical Report. National Aerospace Laboratories, Bangalore, India.
[Department(s): Aerospace Electronics and Controls Division, Aerospace Electronics and Controls Division, Aerospace Electronics and Controls Division]

[] 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.
[Department(s): Flight Mechanics and Control Division, Flight Mechanics and Control Division, Flight Mechanics and Control Division, Other]

[] Girija, G and Raol, JR (1992) PC Based Flight Path Reconstruction using UD Factorization Filtering Algorithm. Technical Report. National Aerospace Laboratories, Bangalore, India.
[Department(s): Flight Mechanics and Control Division, Flight Mechanics and Control Division]

[] Srinathkumar, S and Waszak, Martin R (1992) Active flutter suppression using dipole filters. Technical Report. National Aeronautical Laboratories, Bangalore, India.
[Department(s): Flight Mechanics and Control Division, Other] ["page:no_fulltext_short" not defined]

[] Shyam, Chetty and Raol, JR (1992) Computer aided evaluation aircraft handling qualities and flight control system robustness. In: AIAA atmospheric flight mechanics conference.
[Department(s): Flight Mechanics and Control Division, Flight Mechanics and Control Division]

[] 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.
[Department(s): Other, Systems Engineering Division]

[] Rajamurthy, MS and Basappa, - (1991) NALLA 1 Longitudinal stick-free stability. Technical Report. National Aeronautical Laboratory, Bangalore, India.
[Department(s): Flight Mechanics and Control Division, Flight Mechanics and Control Division]

[] 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.
[Department(s): Flight Mechanics and Control Division, Flight Mechanics and Control Division, Flight Mechanics and Control Division, Flight Mechanics and Control Division]

[] Varute, PT and Gnanesh, N (1991) NALLA prototype flight envelope. Technical Report. National Aerospace Laboratories, Bangalore, India.
[Department(s): Computational and Theoretical Fluid Dynamics Division, Materials Science Division]

[] 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.
[Department(s): Flight Mechanics and Control Division, Flight Mechanics and Control Division, Flight Mechanics and Control Division, Flight Mechanics and Control Division]

[] 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.
[Department(s): Flight Mechanics and Control Division, Flight Mechanics and Control Division, Flight Mechanics and Control Division]

[] Rao, RMVGK (1991) Composite materials indigenisation for FRP - Air crafts. Technical Report. National Aerospace Laboratories, Bangalore, India.
[Department(s): Materials Science Division]

[] Prasad, S Ganesh and Premalatha, - and Ramamoorthy, P (1991) Small Aircraft Stability and Response Analysis (SASTRA). Technical Report. National Aerospace Laboratories, Bangalore, India.
[Department(s): Computational and Theoretical Fluid Dynamics Division, Computational and Theoretical Fluid Dynamics Division, Computational and Theoretical Fluid Dynamics Division]

[] 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.
[Department(s): Flight Mechanics and Control Division, Flight Mechanics and Control Division, Flight Mechanics and Control Division]

[] 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.
[Department(s): Flight Mechanics and Control Division, Flight Mechanics and Control Division]

[] 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.
[Department(s): Flight Mechanics and Control Division, Flight Mechanics and Control Division]

[] 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.
[Department(s): Flight Mechanics and Control Division, Flight Mechanics and Control Division, Flight Mechanics and Control Division, Other]

[] Varute, PT (1990) Precision mechanics of actuators in aircraft and rockets. Technical Report. National Aeronautical Laboratory, Bangalore, India.
[Department(s): Materials Science Division] ["page:no_fulltext_short" not defined]

[] Ramamoorthy, P (1989) Extended Kalman Filter Algorithm (EKF). Technical Report. National Aerospace Laboratories, Bangalore, India.
[Department(s): Computational and Theoretical Fluid Dynamics Division]

[] Chetty, Shyam (1988) Design of robust flight control systems. Technical Report. National Aeronautical Laboratory, Bangalore, India.
[Department(s): Systems Engineering Division]

[] Rajamurthy, MS (1988) Stability and control derivatives of Light Canard Research Aircraft (LCRA). Technical Report. National Aeronautical Laboratory, Bangalore, India.
[Department(s): Systems Engineering Division]

[] Ramamurthy, TV (1988) An automated aid for microcomputer implementation of flight control systems. Technical Report. National Aeronautical Laboratory, Bangalore, India.
[Department(s): Systems Engineering Division]

[] Manoharan, LC and Muthuvel, S (1987) An intelligent fiberoptic data bus for fly-by-light applications. Technical Report. National Aeronautical Laboratory, Bangalore, India.
[Department(s): Systems Engineering Division, Systems Engineering Division]

[] Madhuranath, P and Niranjana, T (1987) Flight data analysis of the short period characteristics of pushpak aircraft. Technical Report. National Aeronautical Laboratory, Bangalore, India.
[Department(s): Systems Engineering Division, Systems Engineering Division]

[] Madhuranath, Padma and Sridhar, JK and Bhagavan, Satya B (1987) Simulation of a Light Aircraft. Technical Report. National Aeronautical Laboratory, Bangalore, India.
[Department(s): Systems Engineering Division, Systems Engineering Division, Systems Engineering Division]

[] 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.
[Department(s): Experimental Aerodynamics Division, Other] ["page:no_fulltext_short" not defined]

[] 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.
[Department(s): Propulsion Division, Other]

[] Varute, PT (1986) Estimates of longitudinal and lateral stability and control characteristics of Pushpak Aircraft. Technical Report. National Aeronautical Laboratory, Bangalore, India.
[Department(s): Systems Engineering Division]

[] 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.
[Department(s): Systems Engineering Division, Systems Engineering Division, Systems Engineering Division]

[] 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.
[Department(s): Other, Systems Engineering Division, Systems Engineering Division, Systems Engineering Division]

[] 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.
[Department(s): Flight Mechanics and Control Division, Other] ["page:no_fulltext_short" not defined]

[] 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.
[Department(s): Systems Engineering Division, Systems Engineering Division, Systems Engineering Division]

[] Madhavan, Chinmayee and Dasannacharya, BS and Rajanna, D and Nagabhushana, S (1985) Aircraft weighing system. Technical Report. National Aeronautical Laboratory, Bangalore, India.
[Department(s): Systems Engineering Division, Systems Engineering Division, Systems Engineering Division, Systems Engineering Division]

[] Sarma, GR (1983) Nonlinear filter for pilot's remnant attenuation. Journal of Guidance, Control and Dynamics, 6 (2). pp. 123-124. ISSN 0731-5090
[Department(s): Systems Engineering Division]

[] 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.
[Department(s): Systems Engineering Division, Systems Engineering Division]

[] Ramabhadran, S and Sridharan, R (1982) Computation of the aerodynamic characteristics of wings in linearised supersonic flow. Technical Report. National Aeronautical Laboratory, Bangalore, India.
[Department(s): Aerodynamics, Aerodynamics]

[] 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
[Department(s): Aerodynamics]

[] Srinivas, K (1980) Computation of steady supersonic flows - two dimentional and axisymmetric. Technical Report. National Aeronautical Laboratory, Bangalore, India.
[Department(s): Computer Support and Services Division]

[] Vepa, R (1979) Comment on 'active flutter control using generalized unsteady aerodynamic theory'. Journal of Guidance and Control, 2. pp. 446-447.
[Department(s): Structures Division]

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

[] 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.
[Department(s): Aerodynamics, Aerodynamics, Aerodynamics, Aerodynamics, Aerodynamics, Aerodynamics]

[] 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
[Department(s): Systems Engineering Division, Other]

[] 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.
[Department(s): Flight Mechanics and Control Division, Other] ["page:no_fulltext_short" not defined]

[] 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.
[Department(s): Aerodynamics]

[] 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.
[Department(s): Materials Science Division, Other, Materials Science Division]

This list was generated on Fri Mar 12 01:04:04 IST 2010.