H. Takano

发表

Modified Proportional Navigation for a Missile with Varying Velocity-Comparison with the Optimal Guidance

Y. Baba, Naoto Dohi, H. Takano, 2004 .

Optimal Spacecraft Transfer Orbit Design Using DRL Algorithm

I. Yamaguchi, H. Takano, Ryo Endo, 2022, 2022 61st Annual Conference of the Society of Instrument and Control Engineers (SICE).

A Note on the Singularity of Modified Proportional Navigation Guidance

I. Yamaguchi, Youhei Shiraishi, H. Takano, 2022, AIAA SCITECH 2022 Forum.

2007 International Conference on Control, Automation and Systems ( (I IC CC CAS S 2007)

Min-Jea Tahk, Sangdeok Park, Pierre Apkarian, 2007 .

Guidance Law Based on Line-of-Sight Rate Information Considering Uncertain Modeled Dynamics

Takeshi Yamasaki, Hiroyuki Takano, Saori Nakagawa, 2018 .

Comparison Study on Disturbance-compensated Intercept Guidance Using Line-of-sight Rate Information against Optimal Guidance

Yohei Shiraishi, Isao Yamaguchi, Saori Nakagawa, 2019, Transactions of the Society of Instrument and Control Engineers.

Disturbance-compensated intercept guidance using line-of-sight rate information

Takeshi Yamasaki, Hiroyuki Takano, Isao Yamaguchi, 2017, 2017 11th Asian Control Conference (ASCC).

Sliding mode-based intercept guidance with uncertainty and disturbance compensation

Takeshi Yamasaki, Hiroyuki Takano, Isao Yamaguchi, 2015, J. Frankl. Inst..

Trajectory Guidance and Control for a Small UAV

Yoichi Sato, Takeshi Yamasaki, Hiroyuki Takano, 2006 .

On an Air-to-Sea Guided Bomb

Hiroyuki Takano, Yoriaki Baba, Kichiro Takao, 1993 .

Handling Assist System for Landing with the Concept of Training Wheels

Takeshi Yamasaki, Hiroyuki Takano, Yoriaki Baba, 2007 .

Handling Assist System Using Dynamic Inversion

Takeshi Yamasaki, Hiroyuki Takano, Yoriaki Baba, 2009 .

Flight Trajectory Tracking System Applied to Inverse Control for Aerobatic Maneuvers

H. Takano, Y. Baba, S. Ochi, 2002 .

Desired trajectory and guidance force generators for an aircraft

Yoriaki Baba, Masaki Sano, Hiroyuki Takano, 1996 .

Guidance and Control System Design for Chase UAV

Keisuke Enomoto, Takeshi Yamasaki, Hiroyuki Takano, 2008 .

Second Order Sliding Mode-Based Intercept Guidance with Uncertainty and Disturbance Compensation

Takeshi Yamasaki, Hiroyuki Takano, S. N. Balakrishnan, 2013 .

Guidance Law for a Flight Vehicle during Boost Phase.

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

Estimation of Missile Flight Distance and Guidance Law during Boost Phase

Hiroyuki Takano, Yoriaki Baba, Naoto Dohi, 2005 .

Modification of Augmented Proportional Navigation for a Missile with Varying Velocity

Hiroyuki Takano, Yoriaki Baba, Naoto Dohi, 2004 .

Guidance Law for a Flight Vehicle after Thrust Cutoff

Yoriaki Baba, Naoto Dohi, Hiroyuki Takano, 2003 .

New guidance law for a missile with varying velocity

Hiroyuki Takano, Yoriaki Baba, Tetsuya Takehira, 1994 .

Modified Command to Line-of-Sight Intercept Guidance for Aircraft Defense

Takeshi Yamasaki, Hiroyuki Takano, S. N. Balakrishnan, 2013 .

A note on the optimal AOTV return

H. Takano, Y. Baba, Y. Baba, 2002, Proceedings of the 41st SICE Annual Conference. SICE 2002..

AIR COMBAT GUIDANCE LAW FOR AN UCAV

Yoriaki Baba, Hiroyuki Takano, Seiji Miyamoto, 2002 .