Solution Manual for Orbital Mechanics for Engineering Students – 4th Edition by Howard Curtis

, SOLUTIONS MANUAL

to accompany


ORBITAL MECHANICS FOR ENGINEERING STUDENTS




Howard D. Curtis
Embry-Riddle Aeronautical University
Daytona Beach, Florida

, Solutions Manual Orbital Mechanics for Engineering Students Chapter 1


Problem 1.1
(a)

 
A  A  Axiˆ  Ay ˆj  Azkˆ  Axiˆ  Ayˆj  Azkˆ 
    
 Axiˆ  Axiˆ  Ayˆj  Azkˆ  Ayˆj  Axiˆ  Ayˆj  Azkˆ  Azkˆ  Axiˆ  Ayˆj  Azkˆ 
     
 Ax2 iˆ  iˆ  Ax Ay iˆ  ˆj  Ax Az iˆ  kˆ   AyAx ˆj  iˆ  Ay2 ˆj  ˆj  AyAz ˆj  kˆ  
   
 
 AzAx kˆ  iˆ  AzAy kˆ  ˆj  Az2 kˆ  kˆ 
 
 Ax2 1  Ax Ay 0  Ax Az 0  Ay Ax 0  Ay2 1  Ay Az 0  Az Ax 0  Az Ay 0  Az2 1
     
2 2 2
 Ax  Ay  Az


But, according to the Pythagorean Theorem, A 2x  A y2  A z2  A2 , where A  A , the magnitude of
the vector A . Thus A  A  A2 .

(b)
iˆ ˆj kˆ
A B  C  A  Bx By Bz
Cx Cy Cz
   
 Ax iˆ  Ay ˆj  Azkˆ  iˆ ByCz  BzCy  ˆjBxCz  BzCx   kˆ BxCy  ByCx 
 
 
 
 Ax ByCz  BzCy  Ay BxC z  BzCx   Az BxCy  ByCx  
or

A  B  C  AxByCz  AyBzCx  AzBxCy  AxBzCy  AyBxC z  AzBy Cx (1)

Note that A  B   C  C  A  B , and according to (1)

C  A  B  CxAyBz  Cy AzBx  Cz AxBy  CxAz By  Cy AxBz  Cz AyBx (2)

The right hand sides of (1) and (2) are identical. Hence A   B  C  A  B  C .

(c)
iˆ ˆj kˆ iˆ ˆj kˆ



A  B  C  Axiˆ  Ayˆj  Azkˆ  Bx  By Bz  Ax Ay Az
Cx Cy Cz ByCz  BzCy BzCx  BxCy BxCy  ByCx


  
 Ay BxCy  ByCx  Az BzCx  BxCz  iˆ  Az ByCz  BzCy  Ax BxCy  ByCx  ˆj
   
  
 A B C  B C   A B C  B C  kˆ

x z x x z y y z z y

 
  
 AyBxCy  AzBxC z  Ay ByCx  AzBz Cx iˆ  AxByCx  AzBy Cz  AxBxCy  Az BzCy ˆj 
 x z x y z y x x z y y z
 A B C  A B C  A B C  A B C kˆ
 Bx AyCy  AzCz   Cx AyBy  AzBz  iˆ  By AxCx  AzCz   Cy AxBx  AzBz  ˆj
   
z x x y y z x x y y
 B A C  A C  C A B  A B  kˆ
 

Add and subtract the underlined terms to get



1

, Solutions Manual Orbital Mechanics for Engineering Students Chapter 1



  
A  B  C   B x A yC y  A zC z  A xC x  C x A yB y  Az B z  A xB x  iˆ
 

  
 By AxCx  AzCz  AyCy  Cy AxBx  AzBz  AyBy  ˆj
 


 y y z z z
 B A C  A C  A C  C A B  A B  A B  kˆ
z x x x x  y y z z



 B x iˆ  B y ˆj  B zk ˆ A Cx x  A yC y  AzCz   C x iˆ  C y ˆj  Czkˆ A xB x  A yB y  AzB z 
or

A  B  C  BA  C  CA  B


Problem 1.2 Using the interchange of Dot and Cross we get

A  B  C  D  A  B  C D
But


A  B  C D   C  A  B D (1)

Using the bac – cab rule on the right, yields

A  B  C D  AC  B  BC  A D

or

A  B  C D  A  DC  B  B  DC  A (2)

Substituting (2) into (1) we get



A  B  C D  A  CB  D  A  DB  C
Problem 1.3

Velocity analysis

From Equation 1.38,

v  vo    rrel  vrel . (1)

From the given information we have

vo  10Iˆ  30Jˆ  5 0 K̂ (2)


   
rrel  r  ro  150Iˆ  200Jˆ  3 0 0 K̂  300Iˆ  200Jˆ  1 0 0 K̂  150Iˆ  400Jˆ  20 0 K̂ (3)



Iˆ Jˆ K̂
  rrel  0.6 0.4 1.0  320Iˆ  270Jˆ  30 0K̂ (4)
150 400 200




2