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specification Element

Specification

Namespace: Empty

Schema: Empty

Type
Parents
Children
NameOccurrencesDescription
Sequence Sequence
      Element environment

Environmental conditions

      Element altitude

Altitude

      Element machNumber

Mach number

      Element angleOfSideslip

Angle of sideslip [deg]

      Choice Choice
            Element angleOfAttack

Angle of attack [deg]

            Element targetCl

Target lift coefficient

      Element pStar[0, 1]

Normalized roll rate [rad/sec]. It is specified around the global x-axis with the aircraft model's global reference point as origin and nondimensionalized by: pStar = p * reference length / flow speed.

      Element qStar[0, 1]

Normalized pitch rate [rad/sec]. It is specified around the global y-axis with the aircraft model's global reference point as origin and nondimensionalized by: qStar = q * reference length / flow speed.

      Element rStar[0, 1]

Normalized yaw rate [rad/sec]. It is specified around the global z-axis with the aircraft model's global reference point as origin and nondimensionalized by: rStar = r * reference length / flow speed.

      Element configuration[0, 1]

Configuration

      Element weightAndBalanceUID[0, 1]

Reference to a weight and balance description

Remarks
Specification of the vehicle properties and dynamics
See Also

Reference

aeroCaseType