The main aim is to develop a much cleaner cost-effective way of power generation method, which in turn helps to bring down global warming as well as reduces the power shortages. The objective is to design, characterization, and testing of control mechanism which is a low cost, compact in size and volume, precisely manufacture and perfectly assemble /aligned to perform the intended function. The control mechanism carries the spring, metal plates and bars, rack and pinion gears, chain drive system, bearings, and small size dc gear motor used to drive DC loads

SAE EFFI-CYCLE event is organized by SAE-INDIA. The challenging task is given to design and fabricate an aerodynamic, ergonomically designed, highly engineered, hybrid and two seater vehicle. The goal of TEAM ANANTYAM is to make best performing EFFICYCLE that will satisfy all SAE EFFICYCLE requirements. The main motto of making this vehicle is to bring green revolution over the world with the help of environment friendly Efficycle.

We secured 14th rank at National level and 1st rank at state level.

Self-balancing robot is based on the principle of Inverted pendulum, which is a two wheel vehicle balances itself up in the vertical position with reference to the ground.To find its stable inverted position, I used a generic feedback controller (i.e. PID controller). According to the situation we have to control both angle of pendulum and position of cart. Mechanical design consist of two stepper motors, one arduino micro-controller, IMU (inertial mass unit) sensor and motor river as a basic need. IMU sensor which consists of accelerometer and gyroscope gives the reference acceleration and angle with respect to ground (vertical). It will be prevented from falling by giving acceleration to the wheels according to its inclination from the vertical. If the bot gets tilts by an angle, than in the frame of the wheels; the center of mass of the bot will experience a pseudo force which will apply a torque opposite to the direction of tilt.

When curved composite laminates are subjected to loads which attempt to unfold the laminate, they generally fail by delamination. Strength and stiffness of the structure are reduced considerably by the presence of delamination. Matrix-cracking is also a major mode of failure in laminated composites.