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Shashi Ranjan Kumar

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Associate Professor

Indian Institute of Technology, Bombay

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Research Interests

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Recent Grants

Grant: Close

Cooperative Nonlinear Guidance Strategies for Simultaneous Interception with Finite-Time Convergence

Open Date: 2019-12-01

Close Date: 2021-12-01

Grant: Close

Development of Flight Guidance and Control System of Aerial Vehicles for Path Following

Open Date: 2017-09-01

Close Date: 2021-09-01

Articles (20)

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Collaborators (2)

Dwaipayan Mukherjee

Assistant Professor

Indian Institute of Technology, Bombay

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Abhinav Sinha

Assistant Professor

University of Cincinnati

UNITED STATES

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ApplyKite TwinLearns as you apply

Make your next move.

Prepare your application

Review drafts before you send them.

Shashi Ranjan Kumar

Research Interests

Make your next move.

Recent Grants

Articles (20)

State-Constrained Cooperative Sliding Mode Guidance Using Barrier Lyapunov Function

Cooperative salvo guidance over leader-Follower network with free-Will arbitrary time convergence

Three-Dimensional Nonlinear Path-Following Guidance with Bounded Input Constraints

Path-following guidance for unmanned aerial vehicle with bounded lateral acceleration

Three-dimensional nonlinear guidance with impact time and field-of-view constraints

Autonomous Docking of Uncrewed Surface Vessel with Stationary and Moving Ships

Three-dimensional Trajectory Tracking for Unmanned Aerial Vehicles Under Motion Constraints

3D Cooperative Salvo against a Stationary Target with Arbitrary Time Consensus

A Nonlinear Control Strategy for Path Following Using Variable Virtual Reference speed

Adaptive super twisting algorithm for nonlinear systems with state constraints: application to three-body engagement

Cooperative Guidance for Aerial Defense in Multiagent Systems

Cooperative Optimal Guidance With Inter-Interceptor Avoidance and Angle Constraints

Cooperative Target Interception in 3-D Engagements Over Switched Dynamic Graphs

Design of Exact-Time Convergent Impact Angle Guidance Laws using Trigonometric Sliding Modes

Deviated Pursuit-Based Impact Time Guidance with Bounded Input

Finite-Time Convergent Integrated Relative Position and Attitude Control for Spacecraft Rendezvous

Impact Time Guidance to Capture Moving Targets in the Presence of Multiple Obstacles

Nonlinear 3D Guidance and Control Strategy for Quadrotor Path Following

Nonlinear Control of a Fully-Actuated UAV

Nonlinear Cooperative Salvo Guidance with Seeker-Limited Interceptors

Collaborators (2)

Dwaipayan Mukherjee

Abhinav Sinha

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