If you made any changes in Pure, your changes will be visible here soon.

Personal profile

Research Interests

TECNOLOGIA ELECTRONICA, CIENCIAS DE LA TECNOLOGIA, CIENCIAS DE LA INGENIERÍA

EDI

  • EDI 9

SNI Level

  • SNI 2

Fingerprint Dive into the research topics where Jorge Ángel Dávila Montoya is active. These topic labels come from the works of this person. Together they form a unique fingerprint.

Controllers Engineering & Materials Science
Observability Engineering & Materials Science
Sliding mode control Engineering & Materials Science
Sliding Mode Observer Mathematics
Linear systems Engineering & Materials Science
Fault detection Engineering & Materials Science
Nonlinear systems Engineering & Materials Science
Sliding Mode Mathematics

Network Recent external collaboration on country level. Dive into details by clicking on the dots.

Research Output 2005 2019

  • 1906 Citations
  • 17 h-Index
  • 53 Paper
  • 29 Article
  • 1 Scientific review

Strong Observability for a Class of Linear Hybrid Systems

Rios, H., Davila, J. & Teel, A. R., 18 Jan 2019, p. 3122-3127. 2809 p.

Research output: Contribution to conferencePaper

A Decoupling Approach to Design Observers for Polytopic Takagi-Sugeno Models Subject to Unknown Inputs

Rebai, S. B., Voos, H., Davila, J. A. & Bejarano, F. J., 9 Aug 2018, p. 1352-1357. 6 p.

Research output: Contribution to conferencePaper

State estimation
Linear matrix inequalities
Nonlinear systems

A Tracking Backstepping Sliding-Mode Control for Spacecraft Rendezvous with a Passive Target

Zenteno-Torres, J., Cieslak, J., Henry, D. & Dávila, J., 31 Oct 2018, p. 69-74. 61 p.

Research output: Contribution to conferencePaper

Space rendezvous
Backstepping
Sliding mode control
Feedback linearization
State feedback
2 Citations (Scopus)

A Two-Step Approach for an Enhanced Quadrotor Attitude Estimation via IMU Data

Chang, J., Cieslak, J., Dávila, J., Zhou, J., Zolghadri, A. & Guo, Z., 1 May 2018, In : IEEE Transactions on Control Systems Technology. p. 1140-1148 1025 p.

Research output: Contribution to journalArticle

Units of measurement
Noise
Nonlinear Dynamics
Accelerometers
Sensors
1 Citation (Scopus)

Low Level Control Architecture for Automatic Takeoff and Landing of Fixed Wing UAV

Manjarrez, H., Davila, J. & Lozano, R., 9 Aug 2018, p. 6737-6742. 6062 p.

Research output: Contribution to conferencePaper

Aircraft