Multi-body dynamic modelling and flight control for an asymmetric variable sweep morphing UAV.
- Published in:
- Aeronautical Journal, 2014, v. 118, n. 1204, p. 683, doi. 10.1017/S000192400000943X
- By:
- Publication type:
- Article
Works matching DE "AILERONS"
Results: 30
1
2
Roll control of a MALE UAV using the adaptive torsion wing.
- Published in:
- Aeronautical Journal, 2013, v. 117, n. 1189, p. 299, doi. 10.1017/S0001924000008009
- By:
- Publication type:
- Article
3
Performance and control optimisations using the adaptive torsion wing.
- Published in:
- Aeronautical Journal, 2012, v. 116, n. 1184, p. 1061, doi. 10.1017/S000192400000748X
- By:
- Publication type:
- Article
4
Optimal wing twist distribution for roll control of MAVs.
- Published in:
- Aeronautical Journal, 2011, v. 115, n. 1172, p. 641, doi. 10.1017/S0001924000006333
- By:
- Publication type:
- Article
5
Identification of a MIMO state space model of an F/A-18 aircraft using a subspace method.
- Published in:
- Aeronautical Journal, 2009, v. 113, n. 1141, p. 183, doi. 10.1017/S0001924000700418
- By:
- Publication type:
- Article
6
High-precision control of nonstationary aircrafts by roll angle.
- Published in:
- Automation & Remote Control, 2013, v. 74, n. 5, p. 875, doi. 10.1134/S0005117913050111
- By:
- Publication type:
- Article
7
Fluid structure interaction of a morphed wind turbine blade.
- Published in:
- International Journal of Energy Research, 2013, v. 37, n. 14, p. 1784, doi. 10.1002/er.2991
- By:
- Publication type:
- Article
8
A Contribution Toward Better Understanding of Overbanking Tendency in Fixed-Wing Aircraft.
- Published in:
- Journal of Aviation Technology & Engineering, 2015, v. 4, n. 2, p. 2, doi. 10.7771/2159-6670.1107
- By:
- Publication type:
- Article
9
AN IMAGE PROCESSING METHOD TO DETERMINE THE DAMPING EFFECT PRESENT IN THE MOMENT OF INERTIA MEASUREMENTS PERFORMED ON AN AILERON.
- Published in:
- Journal of Aeronautics & Space Technologies / Havacilik ve Uzay Teknolojileri Dergisi, 2016, v. 9, n. 1, p. 57
- By:
- Publication type:
- Article
10
KANAT YUNUSLAMASI VE DEĞİŞKEN KANATÇIK AÇILARI SIRASINDA OLUŞAN BÜYÜK GİRDAP OLUŞUMLARININ SİMÜLASYONU.
- Published in:
- Journal of Aeronautics & Space Technologies / Havacilik ve Uzay Teknolojileri Dergisi, 2009, v. 4, n. 1, p. 61
- By:
- Publication type:
- Article
11
Mechanical phenomena in ground run of an aircraft with near-critical slip angles.
- Published in:
- International Applied Mechanics, 2006, v. 42, n. 6, p. 714, doi. 10.1007/s10778-006-0139-3
- By:
- Publication type:
- Article
12
Structural Testbed Design and Testing with Controlled Nonlinearities.
- Published in:
- Sound & Vibration, 2016, v. 50, n. 2, p. 6
- By:
- Publication type:
- Article
13
INVESTIGATION INTO THE PRODUCTION FLAWS IN THIN SOLID CARBON LAMINATES BY USING THE ULTRASONIC PHASED ARRAY METHOD.
- Published in:
- Scientific Journal of Silesian University of Technology. Series Transport / Zeszyty Naukowe Politechniki Slaskiej. Seria Transport, 2018, v. 101, p. 141, doi. 10.20858/sjsutst.2018.101.13
- By:
- Publication type:
- Article
14
Manufacturing Process of High Performance–Low Cost Composite Structures for Light Sport Aircrafts.
- Published in:
- Aerospace (MDPI Publishing), 2019, v. 6, n. 2, p. 11, doi. 10.3390/aerospace6020011
- By:
- Publication type:
- Article
15
Failure Analysis of T-38 Aircraft Burst Hydraulic Aileron Return Line.
- Published in:
- 2012
- By:
- Publication type:
- Abstract
16
Moment-Inertial Factor as a Criterion for Assessing the Dimension of an Aircraft.
- Published in:
- Journal of Applied & Computational Mechanics, 2022, v. 8, n. 4, p. 1307, doi. 10.22055/jacm.2022.39741.3455
- By:
- Publication type:
- Article
17
Investigation of the Three-Dimensional Hinge Moment Characteristics Generated by the ONERA-M6 Wing with an Aileron.
- Published in:
- Advances in Mechanical Engineering (Sage Publications Inc.), 2013, v. 5, p. 1, doi. 10.1155/2013/714168
- By:
- Publication type:
- Article
18
Multidisciplinary Optimal Design of an Active Control System and State Estimator for an Aircraft Wing.
- Published in:
- International Journal on Engineering, Science & Technology (IJonEST), 2021, v. 3, n. 2, p. 133
- By:
- Publication type:
- Article
19
A Method for Aileron Actuator Fault Diagnosis Based on PCA and PGC-SVM.
- Published in:
- Shock & Vibration, 2016, p. 1, doi. 10.1155/2016/4807250
- By:
- Publication type:
- Article
20
STEERING MECHANISM AND EFFORTS ON THE NERVA SPACE LAUNCHER.
- Published in:
- Annals of DAAAM & Proceedings, 2010, p. 387
- By:
- Publication type:
- Article
21
UAV Flight Control System Based on an Intelligent BEL Algorithm.
- Published in:
- International Journal of Advanced Robotic Systems, 2013, v. 10, n. 2, p. 1, doi. 10.5772/53746
- By:
- Publication type:
- Article
22
The Euler and Navier-Stokes solutions of a 3-D wing with aileron.
- Published in:
- Acta Mechanica, 1999, v. 138, n. 1-2, p. 51, doi. 10.1007/BF01179541
- By:
- Publication type:
- Article
23
Tendon-Sheath Mechanisms in Flexible Membrane Wing Mini-UAVs: Control and Performance.
- Published in:
- International Journal of Aerospace Engineering, 2017, p. 1, doi. 10.1155/2017/8181743
- By:
- Publication type:
- Article
24
MODEL OF THE OPERATOR FOR CONTROLLING THE AIRCRAFT WITH MATHEMATICAL MODELLING OF THE MOVEMENT.
- Published in:
- Aerospace Research in Bulgaria, 2019, n. 31, p. 143, doi. 10.3897/arb.v31.e13
- By:
- Publication type:
- Article
25
Mathematical modeling of a V-stack piezoelectric aileron actuation.
- Published in:
- INCAS Bulletin, 2016, v. 8, n. 4, p. 141, doi. 10.13111/2066-8201.2016.8.4.12
- By:
- Publication type:
- Article
26
Numerical and experimental investigation on electromechanical aileron actuation system with joint clearance.
- Published in:
- Journal of Mechanical Science & Technology, 2019, v. 33, n. 2, p. 525, doi. 10.1007/s12206-019-0105-8
- By:
- Publication type:
- Article
27
EXPERIMENTAL INVESTIGATION OF THERMAL COMFORT WITH INNOVATIVE GRILLES IN A REAL SCALE ROOM.
- Published in:
- Mathematical Modeling in Civil Engineering, 2011, n. 1/2, p. 214
- By:
- Publication type:
- Article
28
Transition between Level Flight and Hovering of a Tail-Sitter Vertical Takeoff and Landing Aerial Robot.
- Published in:
- Advanced Robotics, 2010, v. 24, n. 5/6, p. 763, doi. 10.1163/016918610X493570
- By:
- Publication type:
- Article
29
Biomimetic Analysis of Insect Wing Kinematics for Flapping MAVs.
- Published in:
- International Journal of Micro Air Vehicles, 2011, v. 3, n. 1, p. 1, doi. 10.1260/1756-8293.3.1.1
- By:
- Publication type:
- Article
30
COMPARATIVE ANALYSIS OF FINITE ELEMENT MODELS FOR A WING LAYOUT.
- Published in:
- Acta Electrotehnica, 2019, v. 60, n. 1/2, p. 200
- By:
- Publication type:
- Article