✦ LIBER ✦

Design of a helicopter output feedback control law using modal and structured-robustness techniques

✍ Scribed by APKARIAN, P.; CHAMPETIER, C.; MAGNI, J. F.

Book ID: 120034331
Publisher: Taylor and Francis Group
Year: 1989
Tongue: English
Weight: 584 KB
Volume: 50
Category: Article
ISSN: 0020-7179
DOI: 10.1080/00207178908953426

No coin nor oath required. For personal study only.

📜 SIMILAR VOLUMES

Robust fixed structure output feedback f

Robust fixed structure output feedback flight control law synthesis and analysis using singular structured value

✍ Siqueira, Daniel; Paglione, Pedro; Moreira, Fernando J.O. 📂 Article 📅 2013 🏛 Elsevier Science 🌐 English ⚖ 395 KB

VIBRATION CONTROL OF A SMART STRUCTURE U

VIBRATION CONTROL OF A SMART STRUCTURE USING PERIODIC OUTPUT FEEDBACK TECHNIQUE

✍ T. C. Manjunath; B. Bandyopadhyay 📂 Article 📅 2008 🏛 John Wiley and Sons 🌐 English ⚖ 801 KB

Feedback design for robust tracking and

Feedback design for robust tracking and robust stiffness in flight control actuators using a modified QFT technique

✍ Thompson, David F.; Pruyn, John S.; Shukla, Amit 📂 Article 📅 1999 🏛 Taylor and Francis Group 🌐 English ⚖ 632 KB

Design of robust excitation controllers

Design of robust excitation controllers for synchronous generators using the spectral and control-canonical-form methods with output feedback

✍ D.P. Papadopoulos; D.V. Bandekas; J.R. Smith 📂 Article 📅 1993 🏛 Elsevier Science 🌐 English ⚖ 909 KB

The linearized model&g of a synchronous generator with exciter, along with a powerful model order-reduction method and two eficient pole-placing algebraic control methods (i.e. the spectral and control-canonical-form (CCF) using state and/or output feedback) have been presented in systematic and con

Design of a low-sensitivity, minimum nor

Design of a low-sensitivity, minimum norm and structurally constrained control law using eigenstructure assignment

✍ Simon P. Burrows; Ron J. Patton 📂 Article 📅 1991 🏛 John Wiley and Sons 🌐 English ⚖ 491 KB

## Abstract The freedom for eigenvalue assignment in specified areas of the complex plane and of the scope for placing the corresponding eigenvectors is utilized to form an analytical gradient‐based optimization problem which may be used to determine a __low‐sensitivity__ eigenvalue assignment with

[American Institute of Aeronautics and A

[American Institute of Aeronautics and Astronautics AIAA Guidance, Navigation, and Control Conference and Exhibit - Monterey, California ()] AIAA Guidance, Navigation, and Control Conference and Exhibit - Experimental Results on Adaptive Output Feedback Control Using a Laboratory Model Helicopter

✍ Kutay, Ali; Calise, Anthony; Idan, Moshe; Hovakimyan, Naira 📂 Article 📅 2002 🏛 American Institute of Aeronautics and Astronautics ⚖ 409 KB