1. Aircraft Dynamics and Control
Aircraft motion is more complicated than spacecraft motion due to the dependence of forces and moments on attitude and velocity
Typical first investigations of aircraft dynamics and control focuses on the longitudinal and lateral motions of symmetric (left-to-right) aircraft near straight and level flight

2. Motion Equations for a Rigid Aircraftb : _ v = ! + 1 m f a e r o t h u s R i g I S ( ) w [ ] T N n d x p , U l y c
& k ; q A - z 6

3. Reference Frames for Aircraft D&Cl F m , . T y p c s u E h b o g d f 3 - x w V v A 2 z : R = ( ) W 1 k B Ã Á

4. Reference Frames for Aircraft D&C (2)l u s t r a i o n ( f m R . S e g ' F h D y c ) w - p b , k d N z : 1 x v

5. Motion Equations for a Rigid Aircraft (2)y p i c a l k n e m t s v r b w ( Ã ) , h d o Á g 3 - 2 1 q u E f V R ; : 4 5 = +

6. Straight and Level Flightc o r i x = ! [ u w p q y z Á Ã ] F g n d l , f m - k ( ) V E A R

7. Linearized Motion L i n e a r z g b o u t h s d l v ° y m w = 1 2 , p4 ( ) T q c k - : x M [ ] E Á Ã A R

8. Longitudinal Motion L o n g i t u d a l M : E e v r T h s c p , y - x= [ w q z ] A 2 6 4 X Z 1 _ + ( ) b 3 7 5 . m f ;

9. Longitudinal Motion (2): E e v r T h s c p , y - x = [ w q z ] B 2 6 4 X Z 1 _ + 3 7 5 A m f b

10. Longitudinal Motion (3)4 h r e m ) : E v T s c - y p , x = [ w q ] A 2 6 X Z 1 _ + 3 7 5 B

11. Longitudinal Motion (4)B u s i n e J t E x a m p l o f L g d M ( 4 h r ) : - v T c y , A = 2 6 1 9 5 7 8 3 S b k ; z

12. Longitudinal Motion (5)B u s i n e J t E x a m p l o f L g d M ( 4 h r ) c . C b y = 2 6 : 7 5 1 9 3 8 k O v I w , A

13. Longitudinal Motion (6)B u s i n e J t E x a m p l o f L g d M ( 4 h r ) c .
Note Final Time S h o r t - p e i d , a v l y m n s u g f c w = 1 : 2 7 6 8

14. Longitudinal Motion (7)B u s i n e J t E x a m p l o f L g d M ( 4 h r ) c .
Note Final Time L o n g - p e r i d , l h t y a m s u f c w = : 7 4 1 2 5 6 . T

15. Lateral Motion L a t e r l M o i n : A d R u c p s , v y w g x = [ ¢ ÁÃ ] T h m B f z j ; b - D