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Conference Paper

Babu, KR and Sarma, IG and Swamy, KN (1995) Sliding mode estimation scheme for missile homing guidance. In: Automatic Control in Aerospace (Aerospace Control '94). A Postprint Volume from the IFAC Symposium, 12-16 Sept. 1994, Palo Alto, CA, USA, pp. 405-410.

Babu, KR and Sarma, IG and Swamy, KN (1994) Two robust homing missile guidance laws based on sliding mode control theory. In: of National Aerospace and Electronics Conference (NAECON'94), 23-27 May 1994, Dayton, OH, USA, pp. 540-547.

Swamy, KN and Sarma, IG (1989) Performance Of APN Guidance Law In A Two Dimensional Aerial Engagement Scenario. In: IEEE 1989 National Aerospace and Electronics Conference, 1989. NAECON 1989, 22-26 May, Dayton,OH, Vol.1, 209-215.

Journal Article

Bhat, Seetharama M and Bai, Sasi D and Powly, AA and Swamy, KN and Ghose, D (2001) Variable structure controller design with application to missile tracking. In: Journal of Guidance, Control, and Dynamics, 24 (4). p. 859.

Krishnabrahmam, V and Bharadwaj, N and Swamy, KN and Sarma, VVS (2000) Guided missile with an intelligent agent. In: Defence-Science Journal, 50 (1). pp. 25-30.

Asthana, CB and Bhat, MS and Swamy, KN (1997) Low-order output feedback compensator for tracking systems. In: Journal of Guidance, Control, and Dynamics, 20 (6). pp. 1263-1265.

Mishra, SK and Sarma, IG and Swamy, KN (1994) Performance evaluation of two fuzzy-logic-based homing guidance schemes. In: Journal of Guidance, Control, and Dynamics, 17 (6). pp. 1389-1391.

Babu, Ravindra K and Sarma, IG and Swamy, KN (1994) Switched Bias Proportional Navigation for Homing Guidance Against Highly Maneuvering Targets. In: Journal of Guidance, Control, and Dynamics, 17 (6). pp. 1357-1363.