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 ...... hiện toàn bộ