Items where Author is "Balakrishna, S"

Up a level
Export as [feed] RSS 2.0 [feed] RSS 1.0 [feed] Atom
Group by: Item Type | No Grouping
Number of items: 35.

Conference or Workshop Item

Balakrishna, S and Niranjana, T and Rajamurthy, MS and Srinathkumar, S and Rajan, SR and Singh, Suresh K (1993) Estimation of aerodynamic derivatives using Dynamic Wind Tunnel Simulation Technique. In: Symposium on System identification, 24-25 Nov 1993, Bangalore, India.

Srinathkumar, S and Madhuranath, Padma and Girija, G and Niranajana, T and Balakrishna, S (1993) Recent contributions to system theoretic approach to flight mechanics research 13; 13;. In: Proceedings of the International Symposium on Recent Advances in Aerospace Sciences and Engineering, 12-15 Dec 1992, Bangalore, India.

Balakrishna, S and Ganesh, VS and Padma, Madhuranath and Bonde, DH and Handoo, KL (1989) Design,construction and evalution of ISRO-NAL acoustic test facility. In: 39th IAF, International Aeronautical Congress, 8-15 Oct 1988, Bangalore, India.

Balakrishna, S and Niranjana, T (1987) Wind tunnel dynamic flying study of the pitching moment derivatives of the Standard Dynamics Model in active control. In: AIAA Atmospheric Flight Mechanics Conference, 17-19 Aug 1987, United States.

Balakrishna, S and Niranjana, T (1987) Wind tunnel dynamic flying study of the pitching movement derivatives of the standard dynamics model in active control AIAA-87-2626. In: AIAA atmospheric flight mechanics conference.

Sundaramurthy, H and Jategoankar, RV and Balakrishna, S (1978) Dynamic stability measurements from tunnel unsteadiness excited random response AIAA-78-831. In: 10th Aerodynamic Testing Conference.

Journal Article

Balakrishna, S and Raol, JR and Rajamurthy, MS (1983) Contributions of congruent pitch motion cue to human activity in manual control. Automatica, 19 . pp. 749-754. ISSN 0005-1098

Jategaonkar, RV and Raol, JR and Balakrishna, S (1982) Determination of model order for dynamical system. IEEE Transactions on Systems, Man, and Cybernetics, SMC-12 . pp. 56-62.

Balakrishna, S and Santharam, A (1976) One axis artificial feel system (pilot proprioceptive cue forces on aircraft joy stick). Journal of Aeronautical Society of India, 28 . pp. 231-236.

Proj.Doc/Technical Report

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.

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 and Rajamurthy, MS (1991) Dynamic flying investigations on 1/13.5 NALLA Model (Longitudinal Results). Technical Report. National Aeronautical Laboratory, Bangalore, India.

Shantha Kumar, N and Raol, JR and Balakrishna, S (1991) Feasibility study of Analysing ASLVD2 flight data estimation of Aerodynamic Derivatives. Technical Report. NAL.

Rajamurthy, MS and Balakrishna, S (1990) Dynamic wind tunnel testing of a flexible wing model 13; 13;. Technical Report. National Aeronautical Laboratory, Bangalore, India.

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 Raol, JR and Balakrishna, S (1990) Aerodynamic Parameter Estimation For Prithvi From First Flight Test Data Preliminary Results 2. 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.

Balakrishna, S and Niranjana, T (1987) A Low Speed Tunnel Semi Free Dynamic Flying Study of Pitching Derivatives of LCA Delta-5 in Active Control using MLE Procedure. Project Report. National Aerospace Laboratories, Bangalore.

Balakrishna, S and Ganesh, VS and Muralidhar, SJ and Nagabhushana, S and Viswanathan, R and Niranjan, T (1986) Acoustic test facility system description manual. Technical Report. National Aeronautical Laboratory, 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 (1986) A low speed tunnel semi-free dynamic flying study of the high angle of attack pitch derivatives of HF-24 using MILE procedure. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Jategaonkar, RV and Balakrishna, S (1986) Effects of flap position on longitudinal parameters of HFB-320. Technical Report. National Aeronautical Laboratory, Bangalore, India.

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.

Balakrishna, S (1983) A low speed tunnel for studies on active control of scaled models. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Balakrishna, S and Chetty, Shyam (1983) Flow chart for a digital fly by wire control system. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Raol, JR and Balakrishna, S and Viswanatham, M (1980) Effect of pitch motion cue on human operator's performance in compensatory experiments. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Jategaonkar, RV and Balakrishna, S (1978) Full scale fatigue control computer system software development-III. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Varute, PT and Eashwar, T and Srinivasa, A and Balakrishna, S (1976) Development of quick acting valve for plot hypersonic wind tunnel of Indian Institute of Science, Bangalore. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Balakrishna, S (1976) Time domain and time series models for human activity in compensatory tracking experiments. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Mahalingam, V and Srikantan, KV and Balakrishna, S (1975) Modification of the model incidence control system of the NAL 4-ft. trisonic wind tunnel. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Balakrishna, S and Varute, PT and Santharam, A and Samraj, AC and Bakshi, DV (1972) Analysis of linkage for a three degree of freedom motion simulator. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Balakrishna, S and Shaila, MS and Santharam, A (1972) A two channel data processing system for the fixed base research simulator. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Balakrishna, S (1970) Wind tunnel pressure regulating systems. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Balakrishna, S and Srinathkumar, S (1963) Pressure transducers using the linear differential transformer. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Balakrishna, S and Niranjana, T and Rajan, SR Moment stability Derivatives of N A G Missile Configuration-at Low Speed using Semi-free Dynamic Flying. Project Report. NAL, Bangalore.

This list was generated on Sun Apr 20 11:59:41 2014 IST.