Computational model for simulation small testing launcher, technical solution

Wind Influence on Miro-launcher Dynamics Model

“…In the case of large-length missiles, as in ML case, this term can become important, and for airplane configurations. The turbulences model obtained can be added to dynamic flight ML model 6 DOF As shown in [1] and [2], for airplane case, other coupling terms may appear, the use of the linear model is necessary.…”

“…Authors of [1] and [2] developed in case of airplane the linear turbulence models in four points. These models also allow calculation of rotation velocity components , , due to turbulence.…”

“…Starting from the method proposed in [2], in work [3] is developed for rockets a linear model of turbulence in two points which allow deducing of angular velocity of pitch and yaw motion. We briefly present this model in what follows.…”

“…In the case of symmetrical axial configurations, the only one that appears is the term due to the longitudinal velocity angle of pitch/yaw (19),(20), and if the aerodynamic length is small relative to the characteristic length, its influence it is small and to use the linear model not justified. In the case of large-length rockets this term can become important, and for airplane configurations, as shown in [1] and [2] other coupling terms may appear, the use of the linear model being indicated.…”