Myung-Joon Kimy, Wook Hyun Kwony, Yong Ho and Chanho Songz ySchool of...  Home/Search
Context
Related
| isltg.snu.ac.kr/papers/../kp...1997c.ps Cached: PS.gz PS PDF This document uses CoBlitz to cache paper downloads. If your firewall is blocking outgoing connections to port 3125, you can use these links to download local copies.
Image Update HelpPS.gz PS PDF From: isltg.snu.ac.kr/papers/control (more) (Enter author homepages) |
Rate this article:      (best)Comment on this article |
Abstract: Receding horizon predictive control (RHPC) methodology is applied to the design of an autopilot for a bank-to-turn (BTT) missile. The main control objective is high tracking performance for guidance commands. The proposed RHPC-based autopilot consists of the RHPC and the design algorithm of future commands. The design algorithm of future commands determines future guidance commands required in the RHPC. It is based on the first-order approximation of the current guidance commands generated from ... (Update)
Active bibliography (related documents): More All
0.5: A Bayesian Approach to Terrain-Aided Navigation - Niclas Bergman (1997) (Correct)
0.5: Design of Nonlinear Autopilots for High Angle of Attack Missiles - Menon, Yousefpor (1996) (Correct)
0.3: Adaptive Target State Estimation Using Neural Networks - Menon, Sharma (1999) (Correct)
Similar documents based on text: More All
0.4: Blended Homing Guidance Law Using Fuzzy Logic - Menon, Iragavarapu (1998) (Correct)
0.3: New Parametric Affine Modeling and Control for Skid-to-Turn.. - Dongkyoung Chwa And (Correct)
0.3: Design of a STT Missile Autopilot Using Functional.. - Song, Lee, Kim.. (Correct)
BibTeX entry: (Update)
@misc{ kimy-autopilot,
author = "Myung-Joon Kimy",
title = "Autopilot Design for BTT Missiles Using Receding Horizon Predictive Control
Scheme",
url = "citeseer.ist.psu.edu/84681.html" }
Citations (may not include all citations):51 Texas Instruments - Guide - 1991
20 Adaptive Optimal Control (context) - Bitmead, Gevers et al. - 1990
11 Generalized Predictive Control - Part I. The Basic Algorithm (context) - Clarke, Mohtadi et al. - 1987
8 Automatic Control of Aircraft and Missiles (context) - Blakelock - 1991
7 Receding horizon tracking control as a predictive control an.. (context) - Kwon, Byun - 1989
5 Advanced Control Systems Design (context) - Lin - 1994
4 Application of Eigenstructure Assignment to Flight Control (context) - Sobel, Shapiro - 1987
3 An Assessment of Air-to-Air Missile Guidance and Control Tec.. (context) - Cloutier, Evers et al. - 1988
3 A skid-to-turn missile autopilot design : The generalized pr.. (context) - Bendotti, M'Saad - 1993
2 and Control Processing (context) - Lin - 1991
2 Bank-to-Turn Missile Autopilot Design Using Loop Transfer Re.. (context) - Wise - 1990
1 A Receding Horizon Predictive Control and its Related GPC wi.. (context) - Lee, Kwon et al. - 1994
1 Autopilot design for bank-to-turn missiles using LQG/LTR met.. (context) - Sheperd, Valavani - 1988
1 Comparison of Classical and Modern Missile Autopilot Design .. (context) - Arrow, Williams - 1989
1 A general adaptive control structure with a missile applicat.. (context) - Krause, Stein - 1988
1 Modern Control Theory for Design of Autopilots for Bank-to-T.. (context) - Williams, Friedland et al. - 1987
1 Precise Flight-Path Control Using a Predictive Algorithm (context) - Jung, Hess - 1991
1 Optimal Intercept Guidance for Short-Range Tactical Missiles (context) - Cottrell - 1971
Documents on the same site (http://isltg.snu.ac.kr/papers/control.htm):
Intervalwise Receding Horizon H_infinity-Tracking Control.. - Kim, Lee, Lee, Kwon (1996) (Correct)
Bounds in Algebraic Riccati and Lyapunov Equations: A Survey.. - Kwon, Moon, Ahn (1996) (Correct)
Online articles have much greater impact More about CiteSeer.IST Add search form to your site Submit documents Feedback
CiteSeer.IST - Copyright Penn State and NEC