1978
DOI: 10.2514/3.28015
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Simple numerical model for calculation of entry vehicle trim response

Abstract: T HE influence of mass and configurational asymmetries on the dynamics of slender, spinning entry vehicles is an important aspect of vehicle design and performance assessment. High-altitude roll resonance and lower-altitude roll/trim effects influence vehicle loading and attendant impact miss. Descriptions of aerodynamic trim effects on reentry vehicle (RV) angle of attack for vehicles with linear aerodynamics are well known. 1 ' 4 Influence of nonlinear aerodynamics on resonant and nonresonant response have b… Show more

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