Load flight data and estimate G forces during the flight.

Compute the indicated airspeed from true airspeed for a pitot-static airspeed indicator.

Create and analyze a fixed-wing aircraft in MATLAB^® using Cessna C182 geometry and coefficient data.

Convert a fixed-wing aircraft to a linear time invariant (LTI) state-space model for linear analysis.

Construct and define a custom state for a fixed-wing aircraft.

Add time-stamped ephemeris data for a constellation of 24 satellites to a satellite scenario for access analysis.

Compare the orbits predicted by the Two-Body-Keplerian, Simplified General Perturbations-4 (SGP4) and Simplified Deep-Space Perturbations-4 (SDP4) orbit propagators.

Set up access analysis between a ground station and conical sensors onboard a constellation of satellites.

Import a Two-Line Element (TLE) file of a satellite constellation, simulate radar detections of the constellation, and track the constellation.

Perform glide calculations for a Cessna 172.