Pseudo-Spectral MPSP-Based Unified Midcourse and Terminal Guidance for Reentry Targets

A unified optimal guidance scheme is presented in this article for both midcourse and terminal phases combined. It minimizes the total deceleration resulting in enhanced range and/or higher impact velocity, while satisfying the terminal constraints on impact angle and miss distance. State-dependent...

Celý popis

Uloženo v:
Podrobná bibliografie
Vydáno v:IEEE transactions on aerospace and electronic systems Ročník 59; číslo 4; s. 3982 - 3994
Hlavní autoři: Sharma, Prayag, Kumar, Prem, Padhi, Radhakant
Médium: Journal Article
Jazyk:angličtina
Vydáno: New York IEEE 01.08.2023
The Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Témata:
Aerodynamics
Angle-constrained guidance
Cost function
Deceleration
Drag
Force
Impact velocity
midcourse guidance
minimum acceleration guidance
Miss distance
Missiles
model predictive static programming (MPSP) guidance
optimal guidance
Philosophical considerations
Solid modeling
Terminal constraints
Terminal guidance
Three-dimensional displays
ISSN:0018-9251, 1557-9603
On-line přístup:Získat plný text
Tagy: Přidat tag
Žádné tagy, Buďte první, kdo vytvoří štítek k tomuto záznamu!
Popis
Shrnutí:A unified optimal guidance scheme is presented in this article for both midcourse and terminal phases combined. It minimizes the total deceleration resulting in enhanced range and/or higher impact velocity, while satisfying the terminal constraints on impact angle and miss distance. State-dependent terms are included in the cost function of the recently proposed generalized quasi-spectral-model predictive static programming (MPSP) and, because of its similarity with the pseudo-spectral philosophy, it is renamed as "pseudo-spectral MPSP." Extensive simulation studies with different engagement scenarios illustrate the effectiveness of the proposed guidance to engage with incoming high-speed ballistic targets.
Bibliografie:ObjectType-Article-1
SourceType-Scholarly Journals-1
ObjectType-Feature-2
content type line 14
ISSN:0018-9251
1557-9603
DOI:10.1109/TAES.2023.3237796