Flight Parameters

R2026b

Calculate aerospace parameters such as ideal airspeed correction, Mach number, dynamic pressure

Calculate common flight dynamics parameters, such as incidence, sideslip, and airspeed.

Blocks

	Incidence, Sideslip, & Airspeed	Calculate incidence, sideslip, and airspeed
	Dynamic Pressure	Compute dynamic pressure using velocity and air density
	Ideal Airspeed Correction	Calculate equivalent airspeed (EAS), calibrated airspeed (CAS), or true airspeed (TAS) from each other
	Incidence & Airspeed	Calculate incidence and airspeed
	Incidence, Sideslip, & Airspeed	Calculate incidence, sideslip, and airspeed
	Mach Number	Compute Mach number using velocity and speed of sound
	Radius at Geocentric Latitude	Estimate radius of ellipsoid planet at geocentric latitude
	Relative Ratio	Calculate relative atmospheric ratios
	Wind Angular Rates	Calculate wind angular rates from body angular rates, angle of attack, sideslip angle, rate of change of angle of attack, and rate of change of sideslip

Model a Quadcopter Based on Parrot Minidrones

Model a quadcopter in Simulink^® based on Parrot^® minidrones.
- Quadcopter Physical Characteristics
- Quadcopter Control and Sensors
- Quadcopter Airframe
- Quadcopter External Environment
- Quadcopter Visualization

Develop Apollo Lunar Module digital autopilot using Simulink and Aerospace Blockset™.

Model NASA HL-20 lifting body and controller modeled in Simulink and Aerospace Blockset, using FlightGear for visualization.

Address the technical and process challenges of aircraft design using the design of a lightweight aircraft.

Compute the indicated airspeed from true airspeed using the Ideal Airspeed Correction block.

Compute the indicated airspeed from true airspeed using the Ideal Airspeed Correction block.