Small satellites provide flexible and economical cost-effective solutions for research and development in the field of the space industry. It is possible to implement and test various mission algorithms with very few resources available. The stringent requirement of a smaller mass of spacecraft has almost eliminated the use of propulsion systems in small satellites. The smaller mass and size of the spacecraft, on the other hand, make it easier to control and adjust the attitude and orbit of the spacecraft with only magnetic control or inertial control. In this field, there are many attitude and orbit control algorithms and techniques that have already been explored.