Tribunal titular

Cargo

Departamento

Profesor

Presidente

ING.MECANICA,INFORMAT.AEROESP.

GONZALO DE GRADO , JESUS

Secretario

LOPEZ RODRIGUEZ , DEIBI

Vocal

ING.MECANICA,INFORMAT.AEROESP.

MARTINEZ PELLITERO , SUSANA

Tribunal suplente

Cargo

Departamento

Profesor

Presidente

ING.MECANICA,INFORMAT.AEROESP.

PEREZ GARCIA , HILDE

Secretario

ING.MECANICA,INFORMAT.AEROESP.

BARREIRO GARCIA , JOAQUIN

Vocal

ING.MECANICA,INFORMAT.AEROESP.

FERNANDEZ ABIA , ANA ISABEL

Description

Qualification

Oral tests

25%

Mixed tests

75%

Other comments and second call

1. The completion of the requested assignments (individual or group), as well as of the possible field practicals/outings, will be mandatory for the elaboration of the final grade.

2. The elaboration of the final grade, weighted between the assignment and the mixed tests, may be subject to the obtaining of a minimum grade in each of the parts.

3. The completion of lab tasks will be essential in order to be eligible for the evaluation process both in the first and in the second call. The lab exercises will include, as long as the necessary means and facilities are available, the performance of laboratory work of compulsory attendance.

4. In case the work is not delivered for the first call, the maximum grade to be obtained in it may be limited for the second call.

5. The presentations and most of the bibliography used are in English. The exams and evaluation tests may be in Spanish or English, according to the student's preference.

Code
A17707
A17709
A17710
A17711
A17730
B958
B959
B962
B5474
B5477
B5479
C2	CMECES2 That students know how to apply their knowledge to their work or vocation in a professional manner and possess the skills that are usually demonstrated through the development and defense of arguments and the resolution of problems within their area of study.
C5	CMECES5 That students have developed those learning skills necessary to undertake further studies with a high degree of autonomy

Competences
A17707 A17710 A17711 A17730	B958 B959 B962 B5474 B5477 B5479	C2 C5
A17709 A17710 A17711	B958 B959 B962 B5474 B5477 B5479	C2 C5
A17707 A17709 A17710 A17711 A17730	B958 B959 B962 B5474 B5477 B5479	C2 C5

Topic	Sub-topic
Block I: INTRODUCTION AND GENERAL DESCRIPTION OF THE HELICOPTER	Lesson 1: GENERAL CONCEPTS Classification, advantages and disadvantages, main characteristics and future trends.
Block II: ROTOR AERODYNAMICS	Lesson 1: INTRODUCTION Theory of the actuator disc, blade element and combined. Lesson 3: ROTOR AEROMECHANICS
Block III: PERFORMANCE OF ROTARY-WING AIRCRAFTS	Lesson 1: VERTICAL FLIGHT Lesson 2: FORWARD FLIGHT Lesson 3: PERFORMANCE
Block IV: HELICOPTER DESIGN AND OPERATION	Lesson 1: STABILITY AND CONTROL
Block V: AEROSTATS	Lesson 1: BASIC PRINCIPLES Lesson 2: AERODYNAMICS Lesson 3: STABILITY AND CONTROL Lesson 4: CONCEPTUAL DESIGN
Block VI: UNMANNED AIR VEHICLES	Lesson 1: INTRODUCTION Applications, types and main characteristics. Lesson 2: UAS MODELING. KINEMATICS AND DYNAMICS

Methodologies :: Tests
	Class hours	Hours outside the classroom	Total hours
PBL (Problem Based Learning)	20	30	50

Practicals using information and communication technologies (ICTs) in computer rooms	8	12	20
Personal tuition	1	0	1

Lecture	28	48	76

Mixed tests	2.5	0	2.5
Oral tests	0.5	0	0.5

(*)The information in the planning table is for guidance only and does not take into account the heterogeneity of the students.

	Description
PBL (Problem Based Learning)
Practicals using information and communication technologies (ICTs) in computer rooms
Personal tuition
Lecture

Basic	G. A. Khoury, J. D. Gillett, Airship Technology, Cambridge Aerospace Series, Series Number 10, 2008 John Seddon and Simon Newman, Basic Helicopter Aerodynamics, Wiley, 2011 Gordon Leishman, Principles of Helicopter Aerodynamics, Cambridge University Press, 2006 Álvaro Cuerva Tejero et all., Teoría de los Helicópteros, Garceta, 2012 Reg Austin, Unmanned Aircraft Systems: UAVS Design, Development and Deployment, Wiley, 2010

Complementary	Brian L. Stevens, Frank L. Lewis, Eric N. Johnson, Aircraft Control and Simulation: Dynamics, Controls Design, and Autonomous Systems, Wiley, 2015 Carichner, Grant; Nicolai, Leland M., Fundamentals of aircraft and airship design. Vol. 2, Airship design and case studies, AIAA Education, 2013 Gareth D. Padfield, Helicopter Flight Dynamics: Including a Treatment of Tiltrotor Aircraft, Wiley, 2018 Wayne Johnson, Helicopter Theory, Dover, 1994 Randal W. Beard, Timothy W. Mclain, Small Unmanned Aircraft: Theory and Practice, Princeton University Press, 2012