Flight Dynamics and System Identification for Modern Feedback Control

Index

A

accelerometer, 43, 45, 79–81, 83

actuator, 24, 38, 45, 57, 61, 76, 85–86, 88–90

aerodynamic effects vector, 31–32 ?

avionics, 6, 14–16, 24, 43, 75, 80

B

Boltzmann-Hamel equations, 8, 31, 36, 75, 77, 91

C

camera, 20, 43, 77

computer-aided drawing (CAD), 7, 17, 24, 77

controllabililty, 64, 70, 73

coupling matrix, 31–32, 35, 45, 49–50, 56–57, 70, 91–94

E

energy, 7, 27, 31–32, 35, 57, 91–92

equation-error, 38, 41, 49, 52, 64, 82–84, 87–89

Euler angle, 9

ensemble average, 16–18, F-16, 63, 93–96

F

fourier transform, 17

G

gravitational effects vector, 31–32, 35, 45, 50, 56, 64, 92, 94

gyroscope, 14, 16, 18–19, 45, 79–81

K

kinematics, 3, 6, 25, 27, 30, 56–57

kronecker product 31 inertial measurement unit (IMU), 14-15, 79–82