Work

A two-pulse scheme for the time-optimal attitude control of a spinning missile

Year: 1990

Type: conference-paper

Source: Guidance, Navigation and Control Conference

DOI: 10.2514/6.1990-3377

Authors: E. JAHANGIR, R. HOWE

Institution: University of Michigan

Language: English

Topic: Guidance and Control Systems

Subfield: Aerospace Engineering

Field: Engineering

Domain: Physical Sciences

Open Access status: closed

Funder: Air Force Office of Scientific Research

OpenAlex ID: W1966507420

FWCI: 1.394

Cites: 10

Cited by: 2

Related to: 10