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Ananthasayanam, MR and Anilkumar, AK and Adimurthy, V (2012) Relook into the historical progress and philosophy of Indian space exploration. In: 41st Histgory Symposium of the International-Academy-of-Astronautics (IAA), SEP 24-28, 2007, Hyderabad, INDIA, pp. 267-292.
Ananthasayanam, MR and Sarkar, AK and Vohra, Prashant and Bhattacharya, A and Srivastava, R (2004) Estimation of Los Rates and Angles using EKF from Noisy Seeker Measurements. In: International Conference on Signal Processing and Communications:SPCOM '04, 11-14 December, Bangalore, India, pp. 525-529.
Ananthasayanam, MR (2004) Some useful conceptual aspects in flight mechanics. In: 42nd AIAA Aerospace Sciences Meeting and Exhibit, 5 - 8 January 2004, Reno, Nevada, pp. 4884-4894.
Anilkumar, AK and Ananthasayanam, MR and Subba Rao, PV (2003) Simulation of some historical on-orbit breakups using assemble model. In: 41st Aerospace Sciences Meeting and Exhibit 2003, 6-9 January 2003, United States.
Ananthasayanam, MR and Sarkar, AK and Vathsal, S (2002) Improved adaptive estimation of noise covariances in design of trajectory tracking filter. In: AIAA Atmospheric Flight Mechanics Conference and Exhibit 2002, 5 August 2002, United States.
Ananthasayanam, MR and Sarkar, AK and Vathsal, S (2002) Parameter estimation of a flight vehicle using MMLE/BFGS estimator under limited measurements. In: AIAA Atmospheric Flight Mechanics Conference and Exhibit 2002, 5 August 2002, United States.
Ananthasayanam, MR (2002) The intuitive beginning, mathematical framework, and experimental aspects in airplane flight mechanics. In: AIAA Atmospheric Flight Mechanics Conference and Exhibit 2002, 5 August 2002, United States.
Ananthasayanam, MR and Gemson, RMO (2001) A proposal for the presentation of results in estimation theory. In: AIAA Atmospheric Flight Mechanics Conference and Exhibit 2001, 6-9 August 2001, Montreal, Canada.
Ananthasayanam, MR and Mohan, Shyam M and Naik, Naren and Gemson, RMO (2016) A heuristic reference recursive recipe for adaptively tuning the Kalman filter statistics part-1: formulation and simulation studies. In: SADHANA-ACADEMY PROCEEDINGS IN ENGINEERING SCIENCES, 41 (12). pp. 1473-1490.
Mohan, Shyam M and Naik, Naren and Gemson, RMO and Ananthasayanam, MR (2016) A heuristic reference recursive recipe for adaptively tuning the Kalman filter statistics part-2: real data studies. In: SADHANA-ACADEMY PROCEEDINGS IN ENGINEERING SCIENCES, 41 (12). pp. 1491-1507.
Naik, Naren and Vasu, RM and Ananthasayanam, MR (2010) Single-resolution and multiresolution extended-Kalman-filter-based reconstruction approaches to optical refraction tomography. In: Applied Optics, 49 (6). pp. 986-1000.
Sarkar, AK and Ananthasayanam, MR and Srinivasan, T and Kar, PK (2009) Comparison of the Radar and Seeker Modes of Pursuer Guidance. In: Journal of guidance control and dynamics, 32 (6). pp. 1912-1920.
Anilkumar, AK and Ananthasayanam, MR and Subba Rao, PV (2007) A constant gain Kalman filter approach for the prediction of re-entry of risk objects. In: Acta Astronautica, 61 (10). pp. 831-839.
Ananthasayanam, MR and Anilkumar, AK and Subba Rao, PV (2006) New Approach for the Evolution and Expansion of Space Debris Scenario. In: Journal of Spacecraft and Rockets, 43 (6). pp. 1271-1282.
Ananthasayanam, MR and Anilkumar, AK and Rao, Subba PV (2006) A new stochastic impressionistic low Earth model of the space debris scenario. In: Acta Astronauitca, 59 (7). pp. 547-559.
Anilkumar, AK and Ananthasayanam, MR and Rao, PVS (2005) A posterior semi-stochastic low Earth debris on-orbit breakup simulation model. In: Acta Astronautica, 57 (9). pp. 733-746.
Philip, NK and Ananthasayanam, MR (2003) Relative position and attitude estimation and control schemes for the final phase of an autonomous docking mission of spacecraft. In: Acta Astronautica, 52 (7). pp. 511-522.
Ananthasayanam, MR and Narasimha, R (1993) Reference annual atmospheres for midlatitude and tropics. In: Advances in Space Research, 13 (1). pp. 95-104.
Ananthasayanam, MR and Narasimha, R (1987) A Proposed International Tropical Reference Atmosphere up to 1000 km. In: Advances in Space Research, 7 (10). pp. 117-131.
Ananthasayanam, MR and Narasimha, R (1969) Approximate solutions for the structure of shock waves. In: Acta Mechanica, 7 (1). pp. 1-15.
Ganeshan, AS and Ananthasayanam, MR (1997) Simulation and modelling of orbital debris environment by equivalent breakups. In: Advances in Space Research, 19 (2). 309-312 .
