Space and Planetary ScienceSocial Sciences (miscellaneous)Control and Systems EngineeringAerospace EngineeringComputers in Earth SciencesMechanical Engineering
S. Sai Sankalp, Vineet Sharma, Abhyudaya Singh, Aneesh Surendra Salian, G Srinivas
AbstractMissiles and sounding rockets usually deviate from the trajectory due to
unstable roll. Fins with cant angles are generally used to provide a rolling
moment in sounding rockets and missiles to minimize the instability. Inducing a
rolling moment also leads to an increase in the rocket motor’s power consumption
due to the rise in drag, so inducing an optimal rolling moment with a minimal
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