Yoriaki Baba

发表

A Study on a Velocity Control System Design Using the Dynamic Inversion Method

Keisuke Enomoto, Takeshi Yamasaki, Hiroyuki Takano, 2010 .

Dual objective optimization in a 3-D maneuver

Hiroyuki Takano, Yoriaki Baba, 1996 .

Guidance law for a flight vehicle with constant acceleration.

Yoriaki Baba, Makoto Yamaguchi, 1990 .

Automatic Control for Chase Aircraft

Keisuke Enomoto, Takeshi Yamasaki, Hiroyuki Takano, 2006 .

A Velocity and Distance Control System Synthesis Using Dynamic Inversion with PI Control

Keisuke Enomoto, Takeshi Yamasaki, Hiroyuki Takano, 2010 .

Handling Assist System for Landing with the Concept of Training Wheels

Takeshi Yamasaki, Hiroyuki Takano, Yoriaki Baba, 2007 .

Choice of Sampling Period for Minimum-Time Computer Control System

Yoriaki Baba, 1980 .

Guidance Law for a Flight Vehicle after Thrust Cutoff

Yoriaki Baba, Naoto Dohi, Hiroyuki Takano, 2003 .

Generalized guidance law for collision courses

R. M. Howe, Yoriaki Baba, Makoto Yamaguchi, 1993 .

Velocity Control System Design for Leader-Following UAV Using Dynamic Inversion

Keisuke Enomoto, Takeshi Yamasaki, Hiroyuki Takano, 2009 .

Guidance Law for a Flight Vehicle with Constant Acceleration against an Accelerating and Turning Target.

Yoriaki Baba, Takao Tsukazaki, 1994 .

Advanced Pure Pursuit Guidance Via Sliding Mode Approach for Chase UAV

Keisuke Enomoto, Takeshi Yamasaki, Hiroyuki Takano, 2009 .

Trajectory Optimization for an Aircraft with Genetic Algorithm

Hiroyuki Takano, Yoriaki Baba, Shigeki Miki, 2002 .

GUIDANCE AND CONTROL SYSTEM FOR POINTING-DEVICE-CONTROLLED AIRCRAFT

Yoichi Sato, Takeshi Yamasaki, Hiroyuki Takano, 2007 .

On an Air-to-Sea Guided Bomb

Hiroyuki Takano, Yoriaki Baba, Kichiro Takao, 1993 .

Handling Assist System Using Dynamic Inversion

Takeshi Yamasaki, Hiroyuki Takano, Yoriaki Baba, 2009 .

New Guidance Law for Air-to-Air Missile

Yoriaki Baba, Tetsuya Takehira, 1993 .

Robust Path-Following for UAV Using Pure Pursuit Guidance

Takeshi Yamasaki, Hiroyuki Takano, Yoriaki Baba, 2009 .

Given flight trajectory controller for aircraft.

Yoriaki Baba, Seizi Miyamoto, 1990 .

Missile guidance system against a ballistic missile

Hiroyuki Takano, Yoriaki Baba, Kichiro Takao, 1991 .

Desired trajectory and guidance force generators for an aircraft

Yoriaki Baba, Masaki Sano, Hiroyuki Takano, 1996 .

Real-Time Simulation Algorithm for an Aircraft and a Missile

Hiroyuki Takano, Yoriaki Baba, Yukio Ueda, 2002 .

AIR COMBAT GUIDANCE LAW FOR AN UCAV

Yoriaki Baba, Hiroyuki Takano, Seiji Miyamoto, 2002 .

Guidance Law for a Flight Vehicle after Burnout

Yoriaki Baba, Naoto Dohi, Hiroyuki Takano, 2002 .

Guidance Law for a Flight Vehicle during Boost Phase.

Hiroyuki Takano, Yoriaki Baba, Y. Baba, 2000 .

Limit of Sampling Periods for Nonlinear Flight Trajectory Controller of Aircraft.

Yoriaki Baba, Kazuya Satonaka, 1992 .

FLIGHT TRAJECTORY CONTROLLER FOR NONLIMEAR MANEUVER

Hiroyuki Takano, Yoriaki Baba, Masaki Sano, 1995 .

Estimation of Missile Flight Distance and Guidance Law during Boost Phase

Hiroyuki Takano, Yoriaki Baba, Naoto Dohi, 2005 .

Computation of Guidance Gains for Nonlinear Flight Trajectory Tracking Control System.

Hiroyuki Takano, Yoriaki Baba, 1999 .

Guidance and Control System Design for Chase UAV

Keisuke Enomoto, Takeshi Yamasaki, Hiroyuki Takano, 2008 .

Trajectory Guidance and Control for a Small UAV

Yoichi Sato, Takeshi Yamasaki, Hiroyuki Takano, 2006 .

Suboptimal guidance with line-of-sight rate only measurements

R. M. Howe, Yoriaki Baba, R. Howe, 1988 .

Variable Speed Missile Guidance Law Against a Maneuvering Target

Hiroyuki Takano, Yoriaki Baba, Naoto Dohi, 2004 .

A generalized guidance law for collision courses

R. M. Howe, Yoriaki Baba, 1991 .

Guidance law for a flight vehicle against an accelerating and turning target

Yoriaki Baba, Takao Tsukazaki, Kichiro Takao, 1992 .

COMBINED FLIGHT GUIDANCE OPTIMIZATION BY GENETIC PROGRAMMING AND SIMPLEX METHOD

Takeshi Yamasaki, Hiroyuki Takano, Yoriaki Baba, 2007 .

Modification of Augmented Proportional Navigation for a Missile with Varying Velocity

Hiroyuki Takano, Yoriaki Baba, Naoto Dohi, 2004 .

Integrated Navigation System for Embedded Guidance and Control System of a Small Unmanned Aerial Vehicle

Takeshi Yamasaki, Hiroyuki Takano, Yoriaki Baba, 2008 .

New guidance law for a missile with varying velocity

Hiroyuki Takano, Yoriaki Baba, Tetsuya Takehira, 1994 .