(2) Consider the three degrees of freedom (DOFS) longitudinal motion of the aircraft as shown in the figure, where r, and 2 are the body-fixed z and : axes, X and Z are the aerodynamic and propulsive forces in the z, and z, directions, M is aerodynamic and propulsive pitching moment, W = mg is the weight of the aircraft, u and w are the velocity components in the z, and directions, q is the pitching angular velocity, and e is the pitch angle. (a) Use Newton equations of motion and Newton-Euler equations of motion to de- rive the three longitudinal dynamical of motions for the aircraft in the body-fixed coordinate system. W =m

University Physics Volume 1
18th Edition
ISBN:9781938168277
Author:William Moebs, Samuel J. Ling, Jeff Sanny
Publisher:William Moebs, Samuel J. Ling, Jeff Sanny
Chapter2: Vectors
Section: Chapter Questions
Problem 2.10CYU: Check Your Understanding Verify that vector v V obtained in Example 2.14 is indeed a unit vector by...
icon
Related questions
icon
Concept explainers
Question
(2) Consider the three degrees of freedom (DOFS) longitudinal motion of the aircraft as
shown in the figure, where r, and z, are the body-fixed r and z axes, X and Z are
the aerodynamic and propulsive forces in the r, and z, directions, M is aerodynamic
and propulsive pitching moment, W = mg is the weight of the aircraft, u and w are
the velocity components in the z, and 2, directions, q is the pitching angular velocity,
and 0 is the pitch angle.
(a) Use Newton equations of motion and Newton-Euler equations of motion to de-
rive the three longitudinal dynamical of motions for the aircraft in the body-fixed
coordinate system.
wing
Transcribed Image Text:(2) Consider the three degrees of freedom (DOFS) longitudinal motion of the aircraft as shown in the figure, where r, and z, are the body-fixed r and z axes, X and Z are the aerodynamic and propulsive forces in the r, and z, directions, M is aerodynamic and propulsive pitching moment, W = mg is the weight of the aircraft, u and w are the velocity components in the z, and 2, directions, q is the pitching angular velocity, and 0 is the pitch angle. (a) Use Newton equations of motion and Newton-Euler equations of motion to de- rive the three longitudinal dynamical of motions for the aircraft in the body-fixed coordinate system. wing
Expert Solution
trending now

Trending now

This is a popular solution!

steps

Step by step

Solved in 2 steps

Blurred answer
Knowledge Booster
Gravitational Force
Learn more about
Need a deep-dive on the concept behind this application? Look no further. Learn more about this topic, physics and related others by exploring similar questions and additional content below.
Similar questions
  • SEE MORE QUESTIONS
Recommended textbooks for you
University Physics Volume 1
University Physics Volume 1
Physics
ISBN:
9781938168277
Author:
William Moebs, Samuel J. Ling, Jeff Sanny
Publisher:
OpenStax - Rice University
Glencoe Physics: Principles and Problems, Student…
Glencoe Physics: Principles and Problems, Student…
Physics
ISBN:
9780078807213
Author:
Paul W. Zitzewitz
Publisher:
Glencoe/McGraw-Hill
Principles of Physics: A Calculus-Based Text
Principles of Physics: A Calculus-Based Text
Physics
ISBN:
9781133104261
Author:
Raymond A. Serway, John W. Jewett
Publisher:
Cengage Learning