NDLI: Trajectory optimization by Gauss pseudospectral method and it's realization in flight

Content Provider	IEEE Xplore Digital Library
Author	Zhang Hongqian Ma Lei Qian Longjun
Copyright Year	2014
Description	Author affiliation: Sch. of Autom., Nanjing Univ. of Sci. & Technol., Nanjing, China (Zhang Hongqian; Ma Lei; Qian Longjun)
Abstract	This paper discusses a problem of the trajectory optimization and it's realization for the maximum flight range of the missile with constraints on the terminal velocity and angle of flight path. The trajectory optimization is resolved with Gauss pseudospectral method, then the optimized trajectory is taken as a standard trajectory for the autopilot to track and realize in numerical simulation flight of the missile. Aircraft guidance law and autopilot design are discussed about the implementation of the optimized trajectory. Two realization methods namely position tracking and acceleration tracking, are proposed and compared. At last, taking the acceleration tracking method as example, this paper analyzes the effects of autopilot parameter changes.
Starting Page	1007
Ending Page	1012
File Size	313799
Page Count	6
File Format	PDF
ISBN	9789881563873
ISSN	19341768
DOI	10.1109/ChiCC.2014.6896765
Language	English
Publisher	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Publisher Date	2014-07-28
Publisher Place	China
Access Restriction	Subscribed
Rights Holder	TCCT, CAA
Subject Keyword	Missiles Automation Guidance and control Educational institutions Realization of optimized trajectory Trajectory Electronic mail Acceleration Gauss pseudospectral methods Optimization Trajectory optimization
Content Type	Text
Resource Type	Article

Sl.	Authority	Responsibilities	Communication Details
1	Ministry of Education (GoI), Department of Higher Education	Sanctioning Authority	https://www.education.gov.in/ict-initiatives
2	Indian Institute of Technology Kharagpur	Host Institute of the Project: The host institute of the project is responsible for providing infrastructure support and hosting the project	https://www.iitkgp.ac.in
3	National Digital Library of India Office, Indian Institute of Technology Kharagpur	The administrative and infrastructural headquarters of the project	Dr. B. Sutradhar bsutra@ndl.gov.in
4	Project PI / Joint PI	Principal Investigator and Joint Principal Investigators of the project	Dr. B. Sutradhar bsutra@ndl.gov.in Prof. Saswat Chakrabarti will be added soon
5	Website/Portal (Helpdesk)	Queries regarding NDLI and its services	support@ndl.gov.in
6	Contents and Copyright Issues	Queries related to content curation and copyright issues	content@ndl.gov.in
7	National Digital Library of India Club (NDLI Club)	Queries related to NDLI Club formation, support, user awareness program, seminar/symposium, collaboration, social media, promotion, and outreach	clubsupport@ndl.gov.in
8	Digital Preservation Centre (DPC)	Assistance with digitizing and archiving copyright-free printed books	dpc@ndl.gov.in
9	IDR Setup or Support	Queries related to establishment and support of Institutional Digital Repository (IDR) and IDR workshops	idr@ndl.gov.in

Trajectory optimization for Missile-borne SAR imaging phase via Gauss Pseudospectral Method

Midcourse trajectory optimization strategy for air-to-air missile based on Gauss Pseudo-spectral Method

Trajectory optimization of a cruise missile using the Gauss Pseudospectral Method

Launch vehicle ascent trajectory optimization based on modified Gauss Pseudospectral method

Trajectory optimization of continuous-thrust spacecraft roundtrip flights via Pseudospectral method

Optimal feedback reentry guidance of hypersonic vehicle based on improved Gauss pseudospectral method

Rapid gliding trajectory optimization via hp-adaptive pseudospectral method

Coordinated motion planning for multi-robot based on multi-stage Pseudospectral Method

Thrust-aerodynamic-force blended guidance strategy for trajectory control interceptor

Trajectory optimization by Gauss pseudospectral method and it's realization in flight

Similar Documents

Trajectory optimization for Missile-borne SAR imaging phase via Gauss Pseudospectral Method

Midcourse trajectory optimization strategy for air-to-air missile based on Gauss Pseudo-spectral Method

Trajectory optimization of a cruise missile using the Gauss Pseudospectral Method

Launch vehicle ascent trajectory optimization based on modified Gauss Pseudospectral method

Trajectory optimization of continuous-thrust spacecraft roundtrip flights via Pseudospectral method

Optimal feedback reentry guidance of hypersonic vehicle based on improved Gauss pseudospectral method

Rapid gliding trajectory optimization via hp-adaptive pseudospectral method

Coordinated motion planning for multi-robot based on multi-stage Pseudospectral Method

Thrust-aerodynamic-force blended guidance strategy for trajectory control interceptor

Trajectory optimization by Gauss pseudospectral method and it's realization in flight