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6Tdtn adjoint variables associated adjustable coast atmospheric density boundary conditions burnout weight C^cose C22cose components constraints to variations control parameter control variables cos7 cose Cosine drag coefficient equations of motion Error Analysis evaluated f with respect flight path angle given gradient method Ignit influence coefficient relating influence the trajectory integrated Langley Research Center Leondes Mach number major error sources maximum payload minimize the sensitivity mission NASA Norn partial derivatives partial of F perturbation equation relating pitch pitch-up pounds powered stages principal error sources Re-entry F reduce the sensitivity reduction in sensitivity Scout booster second order partial Section sensitivity of terminal Simulated sin7 sinej specific impulse stage burn rate Steepened substituting Eq Sunblazer system variables terminal altitude terminal constraints thrust misalignment TOLIP Trajectory Optimization Trajectory shaping vector of adjoint vector of control vector of system velocity weighted sum