Fumiaki Imado

发表

Optimal thrust design of a missile with a pulse motor

Fumiaki Imado, Takeshi Kuroda, Susumu Miwa, 1989 .

Fighter evasive maneuvers against proportional navigation missile

Fumiaki Imado, Susumu Miwa, 1986 .

Clutter effect on the guidance of a semi-active radar homing missile

Fumiaki Imado, Susumu Miwa, 1985 .

Clutter effect on the miss distance of a radar homing missile

Fumiaki Imado, Susumu Miwa, Takeshi Kuroda, 1987 .

The Application of Modified Output Error Method and Its Verification.

Fumiaki Imado, Yasumasa Koyama, 2000 .

The Threat of Supersonic ASM and a Countermeasure AMM System

Fumiaki Imado, 2003 .

A mid-course guidance law for highly maneuverable thrust vector control missiles

Fumiaki Imado, Takeshi Kuroda, 1997 .

Proportional navigation versus high-g barrel roll maneuvers from optimal control of view

Fumiaki Imado, Sachio Uehara, 1996 .

Optimal terminal trajectories for clutter crossover avoidance of a variable flow ducted rocket missile

Fumiaki Imado, Hiroaki Matsuda, Shoichiro Mihara, 1999 .

An Offset Thruster Roll/Yaw Control System for the Satellite in Mid-Altitude Orbits

Fumiaki Imado, H. Saito, F. Imado, 1976 .

A New Missile Guidance Algorithm Against A Maneuvering Target

Fumiaki Imado, Takeshi Kuroda, Min-jea Tahk, 1998 .

Optimal midcourse guidance for medium-range air-to-air missiles

Fumiaki Imado, Susumu Miwa, Takeshi Kuroda, 1988 .

A Study on Automatic Air Combat Simulation

Fumiaki Imado, Keiichi Furukawa, Yoichiro Ozawa, 2001 .

Advanced missile guidance system against a very high speed maneuvering target

Fumiaki Imado, Takeshi Kuroda, F. Imado, 1989 .

Optimal Thrust Control of a Missile with a Pulse Motor

Fumiaki Imado, Takeshi Kuroda, Susumu Miwa, 1991 .

Design of Controllers for Missile Guidance System

Fumiaki Imado, Toshio Furukawa, F. Imado, 1988 .

Missile guidance algorithm against high-g barrel roll maneuvers

Fumiaki Imado, Susumu Miwa, 1994 .

The modified output error method and its application on inverse problems in aeronautics

Fumiaki Imado, Yasumasa Koyama, 1998 .

Optimal mid-course guidance of variable flow ducted rocket missiles

Fumiaki Imado, Takeshi Kuroda, Hiroaki Matsuda, 1998 .

Clutter Effect on the Miss Distance of a Radar Homing Missile

Fumiaki Imado, Takeshi Kuroda, Susumu Miwa, 1988 .

An efficient guidance algorithm against high-g barrel roll maneuvers

Fumiaki Imado, Susumu Miwa, 1990 .

Advanced missile guidance system against very high speed target

Fumiaki Imado, Takeshi Kuroda, 1988 .

A Method of Automatic Air-Combat Simulation and Assessment

Fumiaki Imado, Toshio Furukawa, Takeshi Kuroda, 1998 .

High-g Barrel Roll Maneuvers Against Proportional Navigation from Optimal Control Viewpoint

Fumiaki Imado, Sachio Uehara, 1998 .

Optimal missile guidance system against a hypersonic target

Fumiaki Imado, Takeshi Kuroda, 1992 .

Optimal midcourse guidance for medium-range air-to-air missiles

Fumiaki Imado, Takeshi Kuroda, Susumu Miwa, 1990 .

OPTIMAL AIRCRAFT MANEUVERS AGAINST TWO PROPORTIONAL NAVIGATION GUIDED MISSILES

Fumiaki Imado, Takeshi Kuroda, 2008 .

A Study on the Applicability of Augmented Proportional Navigation Guidance

Kimio Kanai, Fumiaki Imado, Akira Ichikawa, 1993 .

General Purpose Tactical Missile Simulation Program

Fumiaki Imado, Sadao Akishita, 1980 .

Improved advanced missile guidance system against a hypersonic target with short maneuvering time

Fumiaki Imado, Takeshi Kuroda, 1990 .

An Extended Study on A New Missile Guidance Algorithm Against A Maneuvering Target

Fumiaki Imado, Min-jea Tahk, Makoto Nagayama, 2001 .

Advanced Techniques in Missile Guidance and Control.

Fumiaki Imado, Takeshi Kuroda, Toshio Furukawa, 1993 .

The Application of Modified Output Error Method on ALFLEX Flight Data

Fumiaki Imado, Yasumasa Koyama, 2002 .

A preliminary study on an autonomous future tactical missile

Fumiaki Imado, Takeshi Kuroda, 1991 .

The application of modified output error method and its verification on inverse problems in aeronautics (No.2)

Fumiaki Imado, Yasumasa Koyama, 2000 .